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/*
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* This file is free software : you can redistribute it and / or modify it
* under the terms of the GNU General Public License as published by the
* Free Software Foundation , either version 3 of the License , or
* ( at your option ) any later version .
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*
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* This file is distributed in the hope that it will be useful , but
* WITHOUT ANY WARRANTY ; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE .
* See the GNU General Public License for more details .
*
* You should have received a copy of the GNU General Public License along
* with this program . If not , see < http : //www.gnu.org/licenses/>.
*
* Author : Eugene Shamaev , Siddharth Bharat Purohit
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*/
# include <AP_Common/AP_Common.h>
# include <AP_HAL/AP_HAL.h>
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# if HAL_ENABLE_DRONECAN_DRIVERS
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# include "AP_DroneCAN.h"
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# include <GCS_MAVLink/GCS.h>
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# include <AP_BoardConfig/AP_BoardConfig.h>
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# include <AP_CANManager/AP_CANManager.h>
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# include <AP_Arming/AP_Arming.h>
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# include <AP_GPS/AP_GPS_DroneCAN.h>
# include <AP_Compass/AP_Compass_DroneCAN.h>
# include <AP_Baro/AP_Baro_DroneCAN.h>
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# include <AP_Vehicle/AP_Vehicle.h>
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# include <AP_BattMonitor/AP_BattMonitor_DroneCAN.h>
# include <AP_Airspeed/AP_Airspeed_DroneCAN.h>
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# include <AP_OpticalFlow/AP_OpticalFlow_HereFlow.h>
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# include <AP_RangeFinder/AP_RangeFinder_DroneCAN.h>
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# include <AP_RCProtocol/AP_RCProtocol_DroneCAN.h>
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# include <AP_EFI/AP_EFI_DroneCAN.h>
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# include <AP_GPS/AP_GPS_DroneCAN.h>
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# include <AP_GPS/AP_GPS.h>
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# include <AP_BattMonitor/AP_BattMonitor_DroneCAN.h>
# include <AP_Compass/AP_Compass_DroneCAN.h>
# include <AP_Airspeed/AP_Airspeed_DroneCAN.h>
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# include <AP_Proximity/AP_Proximity_DroneCAN.h>
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# include <SRV_Channel/SRV_Channel.h>
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# include <AP_ADSB/AP_ADSB.h>
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# include "AP_DroneCAN_DNA_Server.h"
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# include <AP_Logger/AP_Logger.h>
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# include <AP_Notify/AP_Notify.h>
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# include <AP_OpenDroneID/AP_OpenDroneID.h>
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# include <AP_Mount/AP_Mount_Xacti.h>
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# include <string.h>
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extern const AP_HAL : : HAL & hal ;
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// setup default pool size
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# ifndef DRONECAN_NODE_POOL_SIZE
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# if HAL_CANFD_SUPPORTED
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# define DRONECAN_NODE_POOL_SIZE 16384
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# else
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# define DRONECAN_NODE_POOL_SIZE 8192
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# endif
# endif
# if HAL_CANFD_SUPPORTED
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# define DRONECAN_STACK_SIZE 8192
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# else
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# define DRONECAN_STACK_SIZE 4096
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# endif
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# ifndef AP_DRONECAN_VOLZ_FEEDBACK_ENABLED
# define AP_DRONECAN_VOLZ_FEEDBACK_ENABLED 0
# endif
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# define AP_DRONECAN_GETSET_TIMEOUT_MS 100 // timeout waiting for response from node after 0.1 sec
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# define debug_dronecan(level_debug, fmt, args...) do { AP::can().log_text(level_debug, "DroneCAN", fmt, ##args); } while (0)
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// Translation of all messages from DroneCAN structures into AP structures is done
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// in AP_DroneCAN and not in corresponding drivers.
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// The overhead of including definitions of DSDL is very high and it is best to
// concentrate in one place.
// table of user settable CAN bus parameters
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const AP_Param : : GroupInfo AP_DroneCAN : : var_info [ ] = {
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// @Param: NODE
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// @DisplayName: DroneCAN node that is used for this network
// @Description: DroneCAN node should be set implicitly
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// @Range: 1 250
// @User: Advanced
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AP_GROUPINFO ( " NODE " , 1 , AP_DroneCAN , _dronecan_node , 10 ) ,
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// @Param: SRV_BM
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// @DisplayName: Output channels to be transmitted as servo over DroneCAN
// @Description: Bitmask with one set for channel to be transmitted as a servo command over DroneCAN
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// @Bitmask: 0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15, 15: Servo 16, 16: Servo 17, 17: Servo 18, 18: Servo 19, 19: Servo 20, 20: Servo 21, 21: Servo 22, 22: Servo 23, 23: Servo 24, 24: Servo 25, 25: Servo 26, 26: Servo 27, 27: Servo 28, 28: Servo 29, 29: Servo 30, 30: Servo 31, 31: Servo 32
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// @User: Advanced
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AP_GROUPINFO ( " SRV_BM " , 2 , AP_DroneCAN , _servo_bm , 0 ) ,
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// @Param: ESC_BM
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// @DisplayName: Output channels to be transmitted as ESC over DroneCAN
// @Description: Bitmask with one set for channel to be transmitted as a ESC command over DroneCAN
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// @Bitmask: 0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16, 16: ESC 17, 17: ESC 18, 18: ESC 19, 19: ESC 20, 20: ESC 21, 21: ESC 22, 22: ESC 23, 23: ESC 24, 24: ESC 25, 25: ESC 26, 26: ESC 27, 27: ESC 28, 28: ESC 29, 29: ESC 30, 30: ESC 31, 31: ESC 32
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// @User: Advanced
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AP_GROUPINFO ( " ESC_BM " , 3 , AP_DroneCAN , _esc_bm , 0 ) ,
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// @Param: SRV_RT
// @DisplayName: Servo output rate
// @Description: Maximum transmit rate for servo outputs
// @Range: 1 200
// @Units: Hz
// @User: Advanced
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AP_GROUPINFO ( " SRV_RT " , 4 , AP_DroneCAN , _servo_rate_hz , 50 ) ,
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// @Param: OPTION
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// @DisplayName: DroneCAN options
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// @Description: Option flags
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// @Bitmask: 0:ClearDNADatabase,1:IgnoreDNANodeConflicts,2:EnableCanfd,3:IgnoreDNANodeUnhealthy,4:SendServoAsPWM,5:SendGNSS,6:UseHimarkServo,7:HobbyWingESC,8:EnableStats
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// @User: Advanced
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AP_GROUPINFO ( " OPTION " , 5 , AP_DroneCAN , _options , 0 ) ,
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// @Param: NTF_RT
// @DisplayName: Notify State rate
// @Description: Maximum transmit rate for Notify State Message
// @Range: 1 200
// @Units: Hz
// @User: Advanced
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AP_GROUPINFO ( " NTF_RT " , 6 , AP_DroneCAN , _notify_state_hz , 20 ) ,
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AP_UAVCAN: added CAN_Dx_UC_ESC_OF parameter
this allows for an offset in ESC numbering for much more efficient CAN
bandwidth usage.
For example, on a coaxial OctoQuad quadplane the ESCs are typically
setup as outputs 5 to 12. An ideal setup is to split these over 2 CAN
buses, with one CAN bus for the top layer and the one bus for the
bottom layer (allowing for VTOL flight with one bus failed).
Without this offset parameter you would be sending RawCommand messages
like this:
bus1: [ 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
bus2: [ 0, 0, 0, 0, 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
this is very wasteful of bus bandwidth, with bus1 using 3x the
bandwidth it should and bus2 using 4x the bandwidth it should (the
above will take 3 can frames for bus1, and 4 can frames for bus 2)
With this patch you can set:
CAN_D1_UC_ESC_OF = 4
CAN_D2_UC_ESC_OF = 8
and you will get this on the bus:
bus1: [ ESC1, ESC2, ESC3, ESC4 ]
bus2: [ ESC1, ESC2, ESC3, ESC4 ]
that takes just 1 can frame per send on each bus
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// @Param: ESC_OF
// @DisplayName: ESC Output channels offset
// @Description: Offset for ESC numbering in DroneCAN ESC RawCommand messages. This allows for more efficient packing of ESC command messages. If your ESCs are on servo functions 5 to 8 and you set this parameter to 4 then the ESC RawCommand will be sent with the first 4 slots filled. This can be used for more efficint usage of CAN bandwidth
// @Range: 0 18
// @User: Advanced
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AP_GROUPINFO ( " ESC_OF " , 7 , AP_DroneCAN , _esc_offset , 0 ) ,
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// @Param: POOL
// @DisplayName: CAN pool size
// @Description: Amount of memory in bytes to allocate for the DroneCAN memory pool. More memory is needed for higher CAN bus loads
// @Range: 1024 16384
// @User: Advanced
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AP_GROUPINFO ( " POOL " , 8 , AP_DroneCAN , _pool_size , DRONECAN_NODE_POOL_SIZE ) ,
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// @Param: ESC_RV
// @DisplayName: Bitmask for output channels for reversible ESCs over DroneCAN.
// @Description: Bitmask with one set for each output channel that uses a reversible ESC over DroneCAN. Reversible ESCs use both positive and negative values in RawCommands, with positive commanding the forward direction and negative commanding the reverse direction.
// @Bitmask: 0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16, 16: ESC 17, 17: ESC 18, 18: ESC 19, 19: ESC 20, 20: ESC 21, 21: ESC 22, 22: ESC 23, 23: ESC 24, 24: ESC 25, 25: ESC 26, 26: ESC 27, 27: ESC 28, 28: ESC 29, 29: ESC 30, 30: ESC 31, 31: ESC 32
// @User: Advanced
AP_GROUPINFO ( " ESC_RV " , 9 , AP_DroneCAN , _esc_rv , 0 ) ,
AP_UAVCAN: added CAN_Dx_UC_ESC_OF parameter
this allows for an offset in ESC numbering for much more efficient CAN
bandwidth usage.
For example, on a coaxial OctoQuad quadplane the ESCs are typically
setup as outputs 5 to 12. An ideal setup is to split these over 2 CAN
buses, with one CAN bus for the top layer and the one bus for the
bottom layer (allowing for VTOL flight with one bus failed).
Without this offset parameter you would be sending RawCommand messages
like this:
bus1: [ 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
bus2: [ 0, 0, 0, 0, 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
this is very wasteful of bus bandwidth, with bus1 using 3x the
bandwidth it should and bus2 using 4x the bandwidth it should (the
above will take 3 can frames for bus1, and 4 can frames for bus 2)
With this patch you can set:
CAN_D1_UC_ESC_OF = 4
CAN_D2_UC_ESC_OF = 8
and you will get this on the bus:
bus1: [ ESC1, ESC2, ESC3, ESC4 ]
bus2: [ ESC1, ESC2, ESC3, ESC4 ]
that takes just 1 can frame per send on each bus
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AP_GROUPEND
} ;
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// this is the timeout in milliseconds for periodic message types. We
// set this to 1 to minimise resend of stale msgs
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# define CAN_PERIODIC_TX_TIMEOUT_MS 2
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AP_DroneCAN : : AP_DroneCAN ( const int driver_index ) :
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_driver_index ( driver_index ) ,
canard_iface ( driver_index ) ,
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_dna_server ( * this , canard_iface , driver_index )
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{
AP_Param : : setup_object_defaults ( this , var_info ) ;
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for ( uint8_t i = 0 ; i < DRONECAN_SRV_NUMBER ; i + + ) {
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_SRV_conf [ i ] . esc_pending = false ;
_SRV_conf [ i ] . servo_pending = false ;
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}
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debug_dronecan ( AP_CANManager : : LOG_INFO , " AP_DroneCAN constructed \n \r " ) ;
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}
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AP_DroneCAN : : ~ AP_DroneCAN ( )
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{
}
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AP_DroneCAN * AP_DroneCAN : : get_dronecan ( uint8_t driver_index )
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{
if ( driver_index > = AP : : can ( ) . get_num_drivers ( ) | |
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AP : : can ( ) . get_driver_type ( driver_index ) ! = AP_CAN : : Protocol : : DroneCAN ) {
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return nullptr ;
}
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return static_cast < AP_DroneCAN * > ( AP : : can ( ) . get_driver ( driver_index ) ) ;
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}
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bool AP_DroneCAN : : add_interface ( AP_HAL : : CANIface * can_iface )
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{
if ( ! canard_iface . add_interface ( can_iface ) ) {
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debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: can't add DroneCAN interface \n \r " ) ;
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return false ;
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}
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return true ;
}
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void AP_DroneCAN : : init ( uint8_t driver_index , bool enable_filters )
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{
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if ( driver_index ! = _driver_index ) {
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debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: init called with wrong driver_index " ) ;
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return ;
}
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if ( _initialized ) {
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debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: init called more than once \n \r " ) ;
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return ;
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}
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node_info_rsp . name . len = hal . util - > snprintf ( ( char * ) node_info_rsp . name . data , sizeof ( node_info_rsp . name . data ) , " org.ardupilot:%u " , driver_index ) ;
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node_info_rsp . software_version . major = AP_DRONECAN_SW_VERS_MAJOR ;
node_info_rsp . software_version . minor = AP_DRONECAN_SW_VERS_MINOR ;
node_info_rsp . hardware_version . major = AP_DRONECAN_HW_VERS_MAJOR ;
node_info_rsp . hardware_version . minor = AP_DRONECAN_HW_VERS_MINOR ;
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# if HAL_CANFD_SUPPORTED
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if ( option_is_set ( Options : : CANFD_ENABLED ) ) {
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canard_iface . set_canfd ( true ) ;
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}
# endif
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uint8_t uid_len = sizeof ( uavcan_protocol_HardwareVersion : : unique_id ) ;
uint8_t unique_id [ sizeof ( uavcan_protocol_HardwareVersion : : unique_id ) ] ;
mem_pool = new uint32_t [ _pool_size / sizeof ( uint32_t ) ] ;
if ( mem_pool = = nullptr ) {
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debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: Failed to allocate memory pool \n \r " ) ;
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return ;
}
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canard_iface . init ( mem_pool , ( _pool_size / sizeof ( uint32_t ) ) * sizeof ( uint32_t ) , _dronecan_node ) ;
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if ( ! hal . util - > get_system_id_unformatted ( unique_id , uid_len ) ) {
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return ;
}
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unique_id [ uid_len - 1 ] + = _dronecan_node ;
memcpy ( node_info_rsp . hardware_version . unique_id , unique_id , uid_len ) ;
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//Start Servers
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if ( ! _dna_server . init ( unique_id , uid_len , _dronecan_node ) ) {
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debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: Failed to start DNA Server \n \r " ) ;
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return ;
}
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// Roundup all subscribers from supported drivers
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# if AP_GPS_DRONECAN_ENABLED
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AP_GPS_DroneCAN : : subscribe_msgs ( this ) ;
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# endif
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# if AP_COMPASS_DRONECAN_ENABLED
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AP_Compass_DroneCAN : : subscribe_msgs ( this ) ;
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# endif
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# if AP_BARO_DRONECAN_ENABLED
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AP_Baro_DroneCAN : : subscribe_msgs ( this ) ;
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# endif
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AP_BattMonitor_DroneCAN : : subscribe_msgs ( this ) ;
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# if AP_AIRSPEED_DRONECAN_ENABLED
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AP_Airspeed_DroneCAN : : subscribe_msgs ( this ) ;
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# endif
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# if AP_OPTICALFLOW_HEREFLOW_ENABLED
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AP_OpticalFlow_HereFlow : : subscribe_msgs ( this ) ;
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# endif
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# if AP_RANGEFINDER_DRONECAN_ENABLED
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AP_RangeFinder_DroneCAN : : subscribe_msgs ( this ) ;
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# endif
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# if AP_RCPROTOCOL_DRONECAN_ENABLED
AP_RCProtocol_DroneCAN : : subscribe_msgs ( this ) ;
# endif
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# if AP_EFI_DRONECAN_ENABLED
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AP_EFI_DroneCAN : : subscribe_msgs ( this ) ;
# endif
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# if AP_PROXIMITY_DRONECAN_ENABLED
AP_Proximity_DroneCAN : : subscribe_msgs ( this ) ;
# endif
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# if HAL_MOUNT_XACTI_ENABLED
AP_Mount_Xacti : : subscribe_msgs ( this ) ;
# endif
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act_out_array . set_timeout_ms ( 5 ) ;
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act_out_array . set_priority ( CANARD_TRANSFER_PRIORITY_HIGH ) ;
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esc_raw . set_timeout_ms ( 2 ) ;
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// esc_raw is one higher than high priority to ensure that it is given higher priority over act_out_array
esc_raw . set_priority ( CANARD_TRANSFER_PRIORITY_HIGH - 1 ) ;
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# if AP_DRONECAN_HOBBYWING_ESC_SUPPORT
esc_hobbywing_raw . set_timeout_ms ( 2 ) ;
esc_hobbywing_raw . set_priority ( CANARD_TRANSFER_PRIORITY_HIGH ) ;
# endif
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# if AP_DRONECAN_HIMARK_SERVO_SUPPORT
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himark_out . set_timeout_ms ( 2 ) ;
himark_out . set_priority ( CANARD_TRANSFER_PRIORITY_HIGH ) ;
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# endif
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rgb_led . set_timeout_ms ( 20 ) ;
rgb_led . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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buzzer . set_timeout_ms ( 20 ) ;
buzzer . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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safety_state . set_timeout_ms ( 20 ) ;
safety_state . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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arming_status . set_timeout_ms ( 20 ) ;
arming_status . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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# if AP_DRONECAN_SEND_GPS
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gnss_fix2 . set_timeout_ms ( 20 ) ;
gnss_fix2 . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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gnss_auxiliary . set_timeout_ms ( 20 ) ;
gnss_auxiliary . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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gnss_heading . set_timeout_ms ( 20 ) ;
gnss_heading . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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gnss_status . set_timeout_ms ( 20 ) ;
gnss_status . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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# endif
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rtcm_stream . set_timeout_ms ( 20 ) ;
rtcm_stream . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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notify_state . set_timeout_ms ( 20 ) ;
notify_state . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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# if HAL_MOUNT_XACTI_ENABLED
xacti_copter_att_status . set_timeout_ms ( 20 ) ;
xacti_copter_att_status . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
xacti_gimbal_control_data . set_timeout_ms ( 20 ) ;
xacti_gimbal_control_data . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
xacti_gnss_status . set_timeout_ms ( 20 ) ;
xacti_gnss_status . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
# endif
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param_save_client . set_timeout_ms ( 20 ) ;
param_save_client . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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param_get_set_client . set_timeout_ms ( 20 ) ;
param_get_set_client . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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node_status . set_priority ( CANARD_TRANSFER_PRIORITY_LOWEST ) ;
node_status . set_timeout_ms ( 1000 ) ;
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protocol_stats . set_priority ( CANARD_TRANSFER_PRIORITY_LOWEST ) ;
protocol_stats . set_timeout_ms ( 3000 ) ;
can_stats . set_priority ( CANARD_TRANSFER_PRIORITY_LOWEST ) ;
can_stats . set_timeout_ms ( 3000 ) ;
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rgb_led . set_timeout_ms ( 20 ) ;
rgb_led . set_priority ( CANARD_TRANSFER_PRIORITY_LOW ) ;
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node_info_server . set_timeout_ms ( 20 ) ;
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// setup node status
node_status_msg . health = UAVCAN_PROTOCOL_NODESTATUS_HEALTH_OK ;
node_status_msg . mode = UAVCAN_PROTOCOL_NODESTATUS_MODE_OPERATIONAL ;
node_status_msg . sub_mode = 0 ;
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// Spin node for device discovery
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for ( uint8_t i = 0 ; i < 5 ; i + + ) {
send_node_status ( ) ;
canard_iface . process ( 1000 ) ;
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}
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hal . util - > snprintf ( _thread_name , sizeof ( _thread_name ) , " dronecan_%u " , driver_index ) ;
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if ( ! hal . scheduler - > thread_create ( FUNCTOR_BIND_MEMBER ( & AP_DroneCAN : : loop , void ) , _thread_name , DRONECAN_STACK_SIZE , AP_HAL : : Scheduler : : PRIORITY_CAN , 0 ) ) {
debug_dronecan ( AP_CANManager : : LOG_ERROR , " DroneCAN: couldn't create thread \n \r " ) ;
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return ;
}
_initialized = true ;
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debug_dronecan ( AP_CANManager : : LOG_INFO , " DroneCAN: init done \n \r " ) ;
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}
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void AP_DroneCAN : : loop ( void )
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{
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while ( true ) {
if ( ! _initialized ) {
hal . scheduler - > delay_microseconds ( 1000 ) ;
continue ;
}
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canard_iface . process ( 1 ) ;
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safety_state_send ( ) ;
notify_state_send ( ) ;
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check_parameter_callback_timeout ( ) ;
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send_parameter_request ( ) ;
send_parameter_save_request ( ) ;
send_node_status ( ) ;
_dna_server . verify_nodes ( ) ;
# if AP_DRONECAN_SEND_GPS
if ( option_is_set ( AP_DroneCAN : : Options : : SEND_GNSS ) & & ! AP_GPS_DroneCAN : : instance_exists ( this ) ) {
// send if enabled and this interface/driver is not used by the AP_GPS driver
gnss_send_fix ( ) ;
gnss_send_yaw ( ) ;
}
# endif
logging ( ) ;
# if AP_DRONECAN_HOBBYWING_ESC_SUPPORT
hobbywing_ESC_update ( ) ;
# endif
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if ( _SRV_armed_mask ! = 0 ) {
// we have active servos
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uint32_t now = AP_HAL : : micros ( ) ;
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const uint32_t servo_period_us = 1000000UL / unsigned ( _servo_rate_hz . get ( ) ) ;
if ( now - _SRV_last_send_us > = servo_period_us ) {
_SRV_last_send_us = now ;
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# if AP_DRONECAN_HIMARK_SERVO_SUPPORT
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if ( option_is_set ( Options : : USE_HIMARK_SERVO ) ) {
SRV_send_himark ( ) ;
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} else
# endif
{
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SRV_send_actuator ( ) ;
}
for ( uint8_t i = 0 ; i < DRONECAN_SRV_NUMBER ; i + + ) {
_SRV_conf [ i ] . servo_pending = false ;
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}
}
}
}
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}
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# if AP_DRONECAN_HOBBYWING_ESC_SUPPORT
void AP_DroneCAN : : hobbywing_ESC_update ( void )
{
uint32_t now = AP_HAL : : millis ( ) ;
if ( now - hobbywing . last_GetId_send_ms > = 1000U ) {
hobbywing . last_GetId_send_ms = now ;
com_hobbywing_esc_GetEscID msg ;
msg . payload . len = 1 ;
msg . payload . data [ 0 ] = 0 ;
esc_hobbywing_GetEscID . broadcast ( msg ) ;
}
}
/*
handle hobbywing GetEscID reply . This gets us the mapping between CAN NodeID and throttle channel
*/
void AP_DroneCAN : : handle_hobbywing_GetEscID ( const CanardRxTransfer & transfer , const com_hobbywing_esc_GetEscID & msg )
{
if ( msg . payload . len = = 2 & &
msg . payload . data [ 0 ] = = transfer . source_node_id ) {
// throttle channel is 2nd payload byte
const uint8_t thr_channel = msg . payload . data [ 1 ] ;
if ( thr_channel > 0 & & thr_channel < = HOBBYWING_MAX_ESC ) {
hobbywing . thr_chan [ thr_channel - 1 ] = transfer . source_node_id ;
}
}
}
/*
find the ESC index given a CAN node ID
*/
bool AP_DroneCAN : : hobbywing_find_esc_index ( uint8_t node_id , uint8_t & esc_index ) const
{
for ( uint8_t i = 0 ; i < HOBBYWING_MAX_ESC ; i + + ) {
if ( hobbywing . thr_chan [ i ] = = node_id ) {
const uint8_t esc_offset = constrain_int16 ( _esc_offset . get ( ) , 0 , DRONECAN_SRV_NUMBER ) ;
esc_index = i + esc_offset ;
return true ;
}
}
return false ;
}
/*
handle hobbywing StatusMsg1 reply
*/
void AP_DroneCAN : : handle_hobbywing_StatusMsg1 ( const CanardRxTransfer & transfer , const com_hobbywing_esc_StatusMsg1 & msg )
{
uint8_t esc_index ;
if ( hobbywing_find_esc_index ( transfer . source_node_id , esc_index ) ) {
update_rpm ( esc_index , msg . rpm ) ;
}
}
/*
handle hobbywing StatusMsg2 reply
*/
void AP_DroneCAN : : handle_hobbywing_StatusMsg2 ( const CanardRxTransfer & transfer , const com_hobbywing_esc_StatusMsg2 & msg )
{
uint8_t esc_index ;
if ( hobbywing_find_esc_index ( transfer . source_node_id , esc_index ) ) {
TelemetryData t {
. temperature_cdeg = int16_t ( msg . temperature * 100 ) ,
. voltage = msg . input_voltage * 0.1f ,
. current = msg . current * 0.1f ,
} ;
update_telem_data ( esc_index , t ,
AP_ESC_Telem_Backend : : TelemetryType : : CURRENT |
AP_ESC_Telem_Backend : : TelemetryType : : VOLTAGE |
AP_ESC_Telem_Backend : : TelemetryType : : TEMPERATURE ) ;
}
}
# endif // AP_DRONECAN_HOBBYWING_ESC_SUPPORT
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void AP_DroneCAN : : send_node_status ( void )
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{
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const uint32_t now = AP_HAL : : millis ( ) ;
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if ( now - _node_status_last_send_ms < 1000 ) {
return ;
}
_node_status_last_send_ms = now ;
node_status_msg . uptime_sec = now / 1000 ;
node_status . broadcast ( node_status_msg ) ;
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if ( option_is_set ( Options : : ENABLE_STATS ) ) {
// also send protocol and can stats
protocol_stats . broadcast ( canard_iface . protocol_stats ) ;
// get can stats
for ( uint8_t i = 0 ; i < canard_iface . num_ifaces ; i + + ) {
if ( canard_iface . ifaces [ i ] = = nullptr ) {
continue ;
}
auto * iface = hal . can [ 0 ] ;
for ( uint8_t j = 0 ; j < HAL_NUM_CAN_IFACES ; j + + ) {
if ( hal . can [ j ] = = canard_iface . ifaces [ i ] ) {
iface = hal . can [ j ] ;
break ;
}
}
auto * bus_stats = iface - > get_statistics ( ) ;
if ( bus_stats = = nullptr ) {
continue ;
}
dronecan_protocol_CanStats can_stats_msg ;
can_stats_msg . interface = i ;
can_stats_msg . tx_requests = bus_stats - > tx_requests ;
can_stats_msg . tx_rejected = bus_stats - > tx_rejected ;
can_stats_msg . tx_overflow = bus_stats - > tx_overflow ;
can_stats_msg . tx_success = bus_stats - > tx_success ;
can_stats_msg . tx_timedout = bus_stats - > tx_timedout ;
can_stats_msg . tx_abort = bus_stats - > tx_abort ;
can_stats_msg . rx_received = bus_stats - > rx_received ;
can_stats_msg . rx_overflow = bus_stats - > rx_overflow ;
can_stats_msg . rx_errors = bus_stats - > rx_errors ;
can_stats_msg . busoff_errors = bus_stats - > num_busoff_err ;
can_stats . broadcast ( can_stats_msg ) ;
}
}
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}
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void AP_DroneCAN : : handle_node_info_request ( const CanardRxTransfer & transfer , const uavcan_protocol_GetNodeInfoRequest & req )
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{
node_info_rsp . status = node_status_msg ;
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node_info_rsp . status . uptime_sec = AP_HAL : : millis ( ) / 1000 ;
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node_info_server . respond ( transfer , node_info_rsp ) ;
}
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int16_t AP_DroneCAN : : scale_esc_output ( uint8_t idx ) {
static const int16_t cmd_max = ( ( 1 < < 13 ) - 1 ) ;
float scaled = 0 ;
//Check if this channel has a reversible ESC. If it does, we can send negative commands.
if ( ( ( ( uint32_t ) 1 ) < < idx ) & _esc_rv ) {
scaled = cmd_max * ( hal . rcout - > scale_esc_to_unity ( _SRV_conf [ idx ] . pulse ) ) ;
} else {
scaled = cmd_max * ( hal . rcout - > scale_esc_to_unity ( _SRV_conf [ idx ] . pulse ) + 1.0 ) / 2.0 ;
scaled = constrain_float ( scaled , 0 , cmd_max ) ;
}
return static_cast < int16_t > ( scaled ) ;
}
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///// SRV output /////
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void AP_DroneCAN : : SRV_send_actuator ( void )
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{
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uint8_t starting_servo = 0 ;
bool repeat_send ;
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WITH_SEMAPHORE ( SRV_sem ) ;
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do {
repeat_send = false ;
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uavcan_equipment_actuator_ArrayCommand msg ;
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uint8_t i ;
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// DroneCAN can hold maximum of 15 commands in one frame
for ( i = 0 ; starting_servo < DRONECAN_SRV_NUMBER & & i < 15 ; starting_servo + + ) {
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uavcan_equipment_actuator_Command cmd ;
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/*
* Servo output uses a range of 1000 - 2000 PWM for scaling .
* This converts output PWM from [ 1000 : 2000 ] range to [ - 1 : 1 ] range that
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* is passed to servo as unitless type via DroneCAN .
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* This approach allows for MIN / TRIM / MAX values to be used fully on
* autopilot side and for servo it should have the setup to provide maximum
* physically possible throws at [ - 1 : 1 ] limits .
*/
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if ( _SRV_conf [ starting_servo ] . servo_pending & & ( ( ( ( uint32_t ) 1 ) < < starting_servo ) & _SRV_armed_mask ) ) {
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cmd . actuator_id = starting_servo + 1 ;
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if ( option_is_set ( Options : : USE_ACTUATOR_PWM ) ) {
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cmd . command_type = UAVCAN_EQUIPMENT_ACTUATOR_COMMAND_COMMAND_TYPE_PWM ;
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cmd . command_value = _SRV_conf [ starting_servo ] . pulse ;
} else {
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cmd . command_type = UAVCAN_EQUIPMENT_ACTUATOR_COMMAND_COMMAND_TYPE_UNITLESS ;
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cmd . command_value = constrain_float ( ( ( float ) _SRV_conf [ starting_servo ] . pulse - 1000.0 ) / 500.0 - 1.0 , - 1.0 , 1.0 ) ;
}
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msg . commands . data [ i ] = cmd ;
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i + + ;
}
}
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msg . commands . len = i ;
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if ( i > 0 ) {
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if ( act_out_array . broadcast ( msg ) > 0 ) {
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_srv_send_count + + ;
} else {
_fail_send_count + + ;
}
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if ( i = = 15 ) {
repeat_send = true ;
}
}
} while ( repeat_send ) ;
}
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# if AP_DRONECAN_HIMARK_SERVO_SUPPORT
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/*
Himark servo output . This uses com . himark . servo . ServoCmd packets
*/
void AP_DroneCAN : : SRV_send_himark ( void )
{
WITH_SEMAPHORE ( SRV_sem ) ;
// ServoCmd can hold maximum of 17 commands. First find the highest pending servo < 17
int8_t highest_to_send = - 1 ;
for ( int8_t i = 16 ; i > = 0 ; i - - ) {
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if ( _SRV_conf [ i ] . servo_pending & & ( ( 1U < < i ) & _SRV_armed_mask ) ! = 0 ) {
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highest_to_send = i ;
break ;
}
}
if ( highest_to_send = = - 1 ) {
// nothing to send
return ;
}
com_himark_servo_ServoCmd msg { } ;
for ( uint8_t i = 0 ; i < = highest_to_send ; i + + ) {
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if ( ( 1U < < i ) & _SRV_armed_mask ) {
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const uint16_t pulse = constrain_int16 ( _SRV_conf [ i ] . pulse - 1000 , 0 , 1000 ) ;
msg . cmd . data [ i ] = pulse ;
}
}
msg . cmd . len = highest_to_send + 1 ;
himark_out . broadcast ( msg ) ;
}
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# endif // AP_DRONECAN_HIMARK_SERVO_SUPPORT
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void AP_DroneCAN : : SRV_send_esc ( void )
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{
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uavcan_equipment_esc_RawCommand esc_msg ;
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uint8_t active_esc_num = 0 , max_esc_num = 0 ;
uint8_t k = 0 ;
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AP_UAVCAN: added CAN_Dx_UC_ESC_OF parameter
this allows for an offset in ESC numbering for much more efficient CAN
bandwidth usage.
For example, on a coaxial OctoQuad quadplane the ESCs are typically
setup as outputs 5 to 12. An ideal setup is to split these over 2 CAN
buses, with one CAN bus for the top layer and the one bus for the
bottom layer (allowing for VTOL flight with one bus failed).
Without this offset parameter you would be sending RawCommand messages
like this:
bus1: [ 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
bus2: [ 0, 0, 0, 0, 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
this is very wasteful of bus bandwidth, with bus1 using 3x the
bandwidth it should and bus2 using 4x the bandwidth it should (the
above will take 3 can frames for bus1, and 4 can frames for bus 2)
With this patch you can set:
CAN_D1_UC_ESC_OF = 4
CAN_D2_UC_ESC_OF = 8
and you will get this on the bus:
bus1: [ ESC1, ESC2, ESC3, ESC4 ]
bus2: [ ESC1, ESC2, ESC3, ESC4 ]
that takes just 1 can frame per send on each bus
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// esc offset allows for efficient packing of higher ESC numbers in RawCommand
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const uint8_t esc_offset = constrain_int16 ( _esc_offset . get ( ) , 0 , DRONECAN_SRV_NUMBER ) ;
AP_UAVCAN: added CAN_Dx_UC_ESC_OF parameter
this allows for an offset in ESC numbering for much more efficient CAN
bandwidth usage.
For example, on a coaxial OctoQuad quadplane the ESCs are typically
setup as outputs 5 to 12. An ideal setup is to split these over 2 CAN
buses, with one CAN bus for the top layer and the one bus for the
bottom layer (allowing for VTOL flight with one bus failed).
Without this offset parameter you would be sending RawCommand messages
like this:
bus1: [ 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
bus2: [ 0, 0, 0, 0, 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
this is very wasteful of bus bandwidth, with bus1 using 3x the
bandwidth it should and bus2 using 4x the bandwidth it should (the
above will take 3 can frames for bus1, and 4 can frames for bus 2)
With this patch you can set:
CAN_D1_UC_ESC_OF = 4
CAN_D2_UC_ESC_OF = 8
and you will get this on the bus:
bus1: [ ESC1, ESC2, ESC3, ESC4 ]
bus2: [ ESC1, ESC2, ESC3, ESC4 ]
that takes just 1 can frame per send on each bus
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// find out how many esc we have enabled and if they are active at all
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for ( uint8_t i = esc_offset ; i < DRONECAN_SRV_NUMBER ; i + + ) {
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if ( ( ( ( uint32_t ) 1 ) < < i ) & _ESC_armed_mask ) {
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max_esc_num = i + 1 ;
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if ( _SRV_conf [ i ] . esc_pending ) {
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active_esc_num + + ;
}
}
}
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// if at least one is active (update) we need to send to all
if ( active_esc_num > 0 ) {
k = 0 ;
2017-04-02 11:55:40 -03:00
AP_UAVCAN: added CAN_Dx_UC_ESC_OF parameter
this allows for an offset in ESC numbering for much more efficient CAN
bandwidth usage.
For example, on a coaxial OctoQuad quadplane the ESCs are typically
setup as outputs 5 to 12. An ideal setup is to split these over 2 CAN
buses, with one CAN bus for the top layer and the one bus for the
bottom layer (allowing for VTOL flight with one bus failed).
Without this offset parameter you would be sending RawCommand messages
like this:
bus1: [ 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
bus2: [ 0, 0, 0, 0, 0, 0, 0, 0, ESC1, ESC2, ESC3, ESC4 ]
this is very wasteful of bus bandwidth, with bus1 using 3x the
bandwidth it should and bus2 using 4x the bandwidth it should (the
above will take 3 can frames for bus1, and 4 can frames for bus 2)
With this patch you can set:
CAN_D1_UC_ESC_OF = 4
CAN_D2_UC_ESC_OF = 8
and you will get this on the bus:
bus1: [ ESC1, ESC2, ESC3, ESC4 ]
bus2: [ ESC1, ESC2, ESC3, ESC4 ]
that takes just 1 can frame per send on each bus
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for ( uint8_t i = esc_offset ; i < max_esc_num & & k < 20 ; i + + ) {
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if ( ( ( ( uint32_t ) 1 ) < < i ) & _ESC_armed_mask ) {
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esc_msg . cmd . data [ k ] = scale_esc_output ( i ) ;
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} else {
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esc_msg . cmd . data [ k ] = static_cast < unsigned > ( 0 ) ;
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}
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k + + ;
}
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esc_msg . cmd . len = k ;
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if ( esc_raw . broadcast ( esc_msg ) ) {
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_esc_send_count + + ;
} else {
_fail_send_count + + ;
}
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// immediately push data to CAN bus
canard_iface . processTx ( true ) ;
}
for ( uint8_t i = 0 ; i < DRONECAN_SRV_NUMBER ; i + + ) {
_SRV_conf [ i ] . esc_pending = false ;
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}
}
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# if AP_DRONECAN_HOBBYWING_ESC_SUPPORT
/*
support for Hobbywing DroneCAN ESCs
*/
void AP_DroneCAN : : SRV_send_esc_hobbywing ( void )
{
com_hobbywing_esc_RawCommand esc_msg ;
uint8_t active_esc_num = 0 , max_esc_num = 0 ;
uint8_t k = 0 ;
// esc offset allows for efficient packing of higher ESC numbers in RawCommand
const uint8_t esc_offset = constrain_int16 ( _esc_offset . get ( ) , 0 , DRONECAN_SRV_NUMBER ) ;
// find out how many esc we have enabled and if they are active at all
for ( uint8_t i = esc_offset ; i < DRONECAN_SRV_NUMBER ; i + + ) {
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if ( ( ( ( uint32_t ) 1 ) < < i ) & _ESC_armed_mask ) {
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max_esc_num = i + 1 ;
if ( _SRV_conf [ i ] . esc_pending ) {
active_esc_num + + ;
}
}
}
// if at least one is active (update) we need to send to all
if ( active_esc_num > 0 ) {
k = 0 ;
for ( uint8_t i = esc_offset ; i < max_esc_num & & k < 20 ; i + + ) {
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if ( ( ( ( uint32_t ) 1 ) < < i ) & _ESC_armed_mask ) {
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esc_msg . command . data [ k ] = scale_esc_output ( i ) ;
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} else {
esc_msg . command . data [ k ] = static_cast < unsigned > ( 0 ) ;
}
k + + ;
}
esc_msg . command . len = k ;
if ( esc_hobbywing_raw . broadcast ( esc_msg ) ) {
_esc_send_count + + ;
} else {
_fail_send_count + + ;
}
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// immediately push data to CAN bus
canard_iface . processTx ( true ) ;
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}
}
# endif // AP_DRONECAN_HOBBYWING_ESC_SUPPORT
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void AP_DroneCAN : : SRV_push_servos ( )
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{
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WITH_SEMAPHORE ( SRV_sem ) ;
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for ( uint8_t i = 0 ; i < DRONECAN_SRV_NUMBER ; i + + ) {
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// Check if this channels has any function assigned
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if ( SRV_Channels : : channel_function ( i ) > = SRV_Channel : : k_none ) {
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_SRV_conf [ i ] . pulse = SRV_Channels : : srv_channel ( i ) - > get_output_pwm ( ) ;
_SRV_conf [ i ] . esc_pending = true ;
_SRV_conf [ i ] . servo_pending = true ;
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}
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}
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uint32_t servo_armed_mask = _servo_bm ;
uint32_t esc_armed_mask = _esc_bm ;
const bool safety_off = hal . util - > safety_switch_state ( ) ! = AP_HAL : : Util : : SAFETY_DISARMED ;
if ( ! safety_off ) {
AP_BoardConfig * boardconfig = AP_BoardConfig : : get_singleton ( ) ;
if ( boardconfig ! = nullptr ) {
const uint32_t safety_mask = boardconfig - > get_safety_mask ( ) ;
servo_armed_mask & = safety_mask ;
esc_armed_mask & = safety_mask ;
} else {
servo_armed_mask = 0 ;
esc_armed_mask = 0 ;
}
}
_SRV_armed_mask = servo_armed_mask ;
_ESC_armed_mask = esc_armed_mask ;
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if ( _ESC_armed_mask ! = 0 ) {
// push ESCs as fast as we can
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# if AP_DRONECAN_HOBBYWING_ESC_SUPPORT
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if ( option_is_set ( Options : : USE_HOBBYWING_ESC ) ) {
SRV_send_esc_hobbywing ( ) ;
} else
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# endif
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{
SRV_send_esc ( ) ;
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}
}
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}
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// notify state send
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void AP_DroneCAN : : notify_state_send ( )
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{
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uint32_t now = AP_HAL : : millis ( ) ;
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if ( _notify_state_hz = = 0 | | ( now - _last_notify_state_ms ) < uint32_t ( 1000 / _notify_state_hz ) ) {
return ;
}
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ardupilot_indication_NotifyState msg ;
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msg . vehicle_state = 0 ;
if ( AP_Notify : : flags . initialising ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_INITIALISING ;
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}
if ( AP_Notify : : flags . armed ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_ARMED ;
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}
if ( AP_Notify : : flags . flying ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_FLYING ;
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}
if ( AP_Notify : : flags . compass_cal_running ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_MAGCAL_RUN ;
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}
if ( AP_Notify : : flags . ekf_bad ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_EKF_BAD ;
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}
if ( AP_Notify : : flags . esc_calibration ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_ESC_CALIBRATION ;
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}
if ( AP_Notify : : flags . failsafe_battery ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_FAILSAFE_BATT ;
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}
if ( AP_Notify : : flags . failsafe_gcs ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_FAILSAFE_GCS ;
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}
if ( AP_Notify : : flags . failsafe_radio ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_FAILSAFE_RADIO ;
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}
if ( AP_Notify : : flags . firmware_update ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_FW_UPDATE ;
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}
if ( AP_Notify : : flags . gps_fusion ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_GPS_FUSION ;
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}
if ( AP_Notify : : flags . gps_glitching ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_GPS_GLITCH ;
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}
if ( AP_Notify : : flags . have_pos_abs ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_POS_ABS_AVAIL ;
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}
if ( AP_Notify : : flags . leak_detected ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_LEAK_DET ;
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}
if ( AP_Notify : : flags . parachute_release ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_CHUTE_RELEASED ;
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}
if ( AP_Notify : : flags . powering_off ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_POWERING_OFF ;
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}
if ( AP_Notify : : flags . pre_arm_check ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_PREARM ;
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}
if ( AP_Notify : : flags . pre_arm_gps_check ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_PREARM_GPS ;
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}
if ( AP_Notify : : flags . save_trim ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_SAVE_TRIM ;
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}
if ( AP_Notify : : flags . vehicle_lost ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_LOST ;
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}
if ( AP_Notify : : flags . video_recording ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_VIDEO_RECORDING ;
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}
if ( AP_Notify : : flags . waiting_for_throw ) {
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msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_THROW_READY ;
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}
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# ifndef HAL_BUILD_AP_PERIPH
const AP_Vehicle * vehicle = AP : : vehicle ( ) ;
if ( vehicle ! = nullptr ) {
if ( vehicle - > is_landing ( ) ) {
msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_IS_LANDING ;
}
if ( vehicle - > is_taking_off ( ) ) {
msg . vehicle_state | = 1 < < ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_STATE_IS_TAKING_OFF ;
}
}
# endif // HAL_BUILD_AP_PERIPH
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msg . aux_data_type = ARDUPILOT_INDICATION_NOTIFYSTATE_VEHICLE_YAW_EARTH_CENTIDEGREES ;
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uint16_t yaw_cd = ( uint16_t ) ( 360.0f - degrees ( AP : : ahrs ( ) . get_yaw ( ) ) ) * 100.0f ;
const uint8_t * data = ( uint8_t * ) & yaw_cd ;
for ( uint8_t i = 0 ; i < 2 ; i + + ) {
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msg . aux_data . data [ i ] = data [ i ] ;
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}
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msg . aux_data . len = 2 ;
notify_state . broadcast ( msg ) ;
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_last_notify_state_ms = AP_HAL : : millis ( ) ;
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}
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# if AP_DRONECAN_SEND_GPS
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void AP_DroneCAN : : gnss_send_fix ( )
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{
const AP_GPS & gps = AP : : gps ( ) ;
const uint32_t gps_lib_time_ms = gps . last_message_time_ms ( ) ;
if ( _gnss . last_gps_lib_fix_ms = = gps_lib_time_ms ) {
return ;
}
_gnss . last_gps_lib_fix_ms = gps_lib_time_ms ;
/*
send Fix2 packet
*/
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uavcan_equipment_gnss_Fix2 pkt { } ;
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const Location & loc = gps . location ( ) ;
const Vector3f & vel = gps . velocity ( ) ;
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pkt . timestamp . usec = AP_HAL : : micros64 ( ) ;
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pkt . gnss_timestamp . usec = gps . time_epoch_usec ( ) ;
if ( pkt . gnss_timestamp . usec = = 0 ) {
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pkt . gnss_time_standard = UAVCAN_EQUIPMENT_GNSS_FIX2_GNSS_TIME_STANDARD_NONE ;
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} else {
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pkt . gnss_time_standard = UAVCAN_EQUIPMENT_GNSS_FIX2_GNSS_TIME_STANDARD_UTC ;
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}
pkt . longitude_deg_1e8 = uint64_t ( loc . lng ) * 10ULL ;
pkt . latitude_deg_1e8 = uint64_t ( loc . lat ) * 10ULL ;
pkt . height_ellipsoid_mm = loc . alt * 10 ;
pkt . height_msl_mm = loc . alt * 10 ;
for ( uint8_t i = 0 ; i < 3 ; i + + ) {
pkt . ned_velocity [ i ] = vel [ i ] ;
}
pkt . sats_used = gps . num_sats ( ) ;
switch ( gps . status ( ) ) {
case AP_GPS : : GPS_Status : : NO_GPS :
case AP_GPS : : GPS_Status : : NO_FIX :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_NO_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_SINGLE ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_DGPS_OTHER ;
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break ;
case AP_GPS : : GPS_Status : : GPS_OK_FIX_2D :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_2D_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_SINGLE ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_DGPS_OTHER ;
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break ;
case AP_GPS : : GPS_Status : : GPS_OK_FIX_3D :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_3D_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_SINGLE ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_DGPS_OTHER ;
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break ;
case AP_GPS : : GPS_Status : : GPS_OK_FIX_3D_DGPS :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_3D_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_DGPS ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_DGPS_SBAS ;
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break ;
case AP_GPS : : GPS_Status : : GPS_OK_FIX_3D_RTK_FLOAT :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_3D_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_RTK ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_RTK_FLOAT ;
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break ;
case AP_GPS : : GPS_Status : : GPS_OK_FIX_3D_RTK_FIXED :
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pkt . status = UAVCAN_EQUIPMENT_GNSS_FIX2_STATUS_3D_FIX ;
pkt . mode = UAVCAN_EQUIPMENT_GNSS_FIX2_MODE_RTK ;
pkt . sub_mode = UAVCAN_EQUIPMENT_GNSS_FIX2_SUB_MODE_RTK_FIXED ;
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break ;
}
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pkt . covariance . len = 6 ;
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float hacc ;
if ( gps . horizontal_accuracy ( hacc ) ) {
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pkt . covariance . data [ 0 ] = pkt . covariance . data [ 1 ] = sq ( hacc ) ;
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}
float vacc ;
if ( gps . vertical_accuracy ( vacc ) ) {
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pkt . covariance . data [ 2 ] = sq ( vacc ) ;
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}
float sacc ;
if ( gps . speed_accuracy ( sacc ) ) {
const float vc3 = sq ( sacc ) ;
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pkt . covariance . data [ 3 ] = pkt . covariance . data [ 4 ] = pkt . covariance . data [ 5 ] = vc3 ;
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}
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gnss_fix2 . broadcast ( pkt ) ;
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const uint32_t now_ms = AP_HAL : : millis ( ) ;
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if ( now_ms - _gnss . last_send_status_ms > = 1000 ) {
_gnss . last_send_status_ms = now_ms ;
/*
send aux packet
*/
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uavcan_equipment_gnss_Auxiliary pkt_auxiliary { } ;
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pkt_auxiliary . hdop = gps . get_hdop ( ) * 0.01 ;
pkt_auxiliary . vdop = gps . get_vdop ( ) * 0.01 ;
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gnss_auxiliary . broadcast ( pkt_auxiliary ) ;
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/*
send Status packet
*/
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ardupilot_gnss_Status pkt_status { } ;
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pkt_status . healthy = gps . is_healthy ( ) ;
if ( gps . logging_present ( ) & & gps . logging_enabled ( ) & & ! gps . logging_failed ( ) ) {
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pkt_status . status | = ARDUPILOT_GNSS_STATUS_STATUS_LOGGING ;
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}
uint8_t idx ; // unused
if ( pkt_status . healthy & & ! gps . first_unconfigured_gps ( idx ) ) {
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pkt_status . status | = ARDUPILOT_GNSS_STATUS_STATUS_ARMABLE ;
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}
uint32_t error_codes ;
if ( gps . get_error_codes ( error_codes ) ) {
pkt_status . error_codes = error_codes ;
}
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gnss_status . broadcast ( pkt_status ) ;
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}
}
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void AP_DroneCAN : : gnss_send_yaw ( )
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{
const AP_GPS & gps = AP : : gps ( ) ;
if ( ! gps . have_gps_yaw ( ) ) {
return ;
}
float yaw_deg , yaw_acc_deg ;
uint32_t yaw_time_ms ;
if ( ! gps . gps_yaw_deg ( yaw_deg , yaw_acc_deg , yaw_time_ms ) & & yaw_time_ms ! = _gnss . last_lib_yaw_time_ms ) {
return ;
}
_gnss . last_lib_yaw_time_ms = yaw_time_ms ;
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ardupilot_gnss_Heading pkt_heading { } ;
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pkt_heading . heading_valid = true ;
pkt_heading . heading_accuracy_valid = is_positive ( yaw_acc_deg ) ;
pkt_heading . heading_rad = radians ( yaw_deg ) ;
pkt_heading . heading_accuracy_rad = radians ( yaw_acc_deg ) ;
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gnss_heading . broadcast ( pkt_heading ) ;
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}
# endif // AP_DRONECAN_SEND_GPS
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// SafetyState send
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void AP_DroneCAN : : safety_state_send ( )
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{
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uint32_t now = AP_HAL : : millis ( ) ;
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if ( now - _last_safety_state_ms < 500 ) {
// update at 2Hz
return ;
}
_last_safety_state_ms = now ;
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{ // handle SafetyState
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ardupilot_indication_SafetyState safety_msg ;
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auto state = hal . util - > safety_switch_state ( ) ;
if ( _SRV_armed_mask ! = 0 | | _ESC_armed_mask ! = 0 ) {
// if we are outputting any servos or ESCs due to
// BRD_SAFETY_MASK then we need to advertise safety as
// off, this changes LEDs to indicate unsafe and allows
// AP_Periph ESCs and servos to run
state = AP_HAL : : Util : : SAFETY_ARMED ;
}
switch ( state ) {
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case AP_HAL : : Util : : SAFETY_ARMED :
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safety_msg . status = ARDUPILOT_INDICATION_SAFETYSTATE_STATUS_SAFETY_OFF ;
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safety_state . broadcast ( safety_msg ) ;
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break ;
case AP_HAL : : Util : : SAFETY_DISARMED :
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safety_msg . status = ARDUPILOT_INDICATION_SAFETYSTATE_STATUS_SAFETY_ON ;
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safety_state . broadcast ( safety_msg ) ;
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break ;
default :
// nothing to send
break ;
}
}
{ // handle ArmingStatus
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uavcan_equipment_safety_ArmingStatus arming_msg ;
arming_msg . status = hal . util - > get_soft_armed ( ) ? UAVCAN_EQUIPMENT_SAFETY_ARMINGSTATUS_STATUS_FULLY_ARMED :
UAVCAN_EQUIPMENT_SAFETY_ARMINGSTATUS_STATUS_DISARMED ;
arming_status . broadcast ( arming_msg ) ;
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}
}
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/*
handle Button message
*/
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void AP_DroneCAN : : handle_button ( const CanardRxTransfer & transfer , const ardupilot_indication_Button & msg )
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{
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switch ( msg . button ) {
case ARDUPILOT_INDICATION_BUTTON_BUTTON_SAFETY : {
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AP_BoardConfig * brdconfig = AP_BoardConfig : : get_singleton ( ) ;
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if ( brdconfig & & brdconfig - > safety_button_handle_pressed ( msg . press_time ) ) {
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AP_HAL : : Util : : safety_state state = hal . util - > safety_switch_state ( ) ;
if ( state = = AP_HAL : : Util : : SAFETY_ARMED ) {
hal . rcout - > force_safety_on ( ) ;
} else {
hal . rcout - > force_safety_off ( ) ;
}
}
break ;
}
}
}
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/*
handle traffic report
*/
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void AP_DroneCAN : : handle_traffic_report ( const CanardRxTransfer & transfer , const ardupilot_equipment_trafficmonitor_TrafficReport & msg )
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{
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# if HAL_ADSB_ENABLED
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AP_ADSB * adsb = AP : : ADSB ( ) ;
if ( ! adsb | | ! adsb - > enabled ( ) ) {
// ADSB not enabled
return ;
}
AP_ADSB : : adsb_vehicle_t vehicle ;
mavlink_adsb_vehicle_t & pkt = vehicle . info ;
pkt . ICAO_address = msg . icao_address ;
pkt . tslc = msg . tslc ;
pkt . lat = msg . latitude_deg_1e7 ;
pkt . lon = msg . longitude_deg_1e7 ;
pkt . altitude = msg . alt_m * 1000 ;
pkt . heading = degrees ( msg . heading ) * 100 ;
pkt . hor_velocity = norm ( msg . velocity [ 0 ] , msg . velocity [ 1 ] ) * 100 ;
pkt . ver_velocity = - msg . velocity [ 2 ] * 100 ;
pkt . squawk = msg . squawk ;
for ( uint8_t i = 0 ; i < 9 ; i + + ) {
pkt . callsign [ i ] = msg . callsign [ i ] ;
}
pkt . emitter_type = msg . traffic_type ;
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if ( msg . alt_type = = ARDUPILOT_EQUIPMENT_TRAFFICMONITOR_TRAFFICREPORT_ALT_TYPE_PRESSURE_AMSL ) {
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pkt . flags | = ADSB_FLAGS_VALID_ALTITUDE ;
pkt . altitude_type = ADSB_ALTITUDE_TYPE_PRESSURE_QNH ;
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} else if ( msg . alt_type = = ARDUPILOT_EQUIPMENT_TRAFFICMONITOR_TRAFFICREPORT_ALT_TYPE_WGS84 ) {
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pkt . flags | = ADSB_FLAGS_VALID_ALTITUDE ;
pkt . altitude_type = ADSB_ALTITUDE_TYPE_GEOMETRIC ;
}
if ( msg . lat_lon_valid ) {
pkt . flags | = ADSB_FLAGS_VALID_COORDS ;
}
if ( msg . heading_valid ) {
pkt . flags | = ADSB_FLAGS_VALID_HEADING ;
}
if ( msg . velocity_valid ) {
pkt . flags | = ADSB_FLAGS_VALID_VELOCITY ;
}
if ( msg . callsign_valid ) {
pkt . flags | = ADSB_FLAGS_VALID_CALLSIGN ;
}
if ( msg . ident_valid ) {
pkt . flags | = ADSB_FLAGS_VALID_SQUAWK ;
}
if ( msg . simulated_report ) {
pkt . flags | = ADSB_FLAGS_SIMULATED ;
}
if ( msg . vertical_velocity_valid ) {
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pkt . flags | = ADSB_FLAGS_VERTICAL_VELOCITY_VALID ;
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}
if ( msg . baro_valid ) {
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pkt . flags | = ADSB_FLAGS_BARO_VALID ;
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}
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vehicle . last_update_ms = AP_HAL : : millis ( ) - ( vehicle . info . tslc * 1000 ) ;
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adsb - > handle_adsb_vehicle ( vehicle ) ;
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# endif
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}
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/*
handle actuator status message
*/
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void AP_DroneCAN : : handle_actuator_status ( const CanardRxTransfer & transfer , const uavcan_equipment_actuator_Status & msg )
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{
// log as CSRV message
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AP : : logger ( ) . Write_ServoStatus ( AP_HAL : : micros64 ( ) ,
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msg . actuator_id ,
msg . position ,
msg . force ,
msg . speed ,
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msg . power_rating_pct ,
0 , 0 , 0 , 0 , 0 , 0 ) ;
}
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# if AP_DRONECAN_HIMARK_SERVO_SUPPORT
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/*
handle himark ServoInfo message
*/
void AP_DroneCAN : : handle_himark_servoinfo ( const CanardRxTransfer & transfer , const com_himark_servo_ServoInfo & msg )
{
// log as CSRV message
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AP : : logger ( ) . Write_ServoStatus ( AP_HAL : : micros64 ( ) ,
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msg . servo_id ,
msg . pos_sensor * 0.01 ,
0 ,
0 ,
0 ,
msg . pos_cmd * 0.01 ,
msg . voltage * 0.01 ,
msg . current * 0.01 ,
msg . motor_temp * 0.2 - 40 ,
msg . pcb_temp * 0.2 - 40 ,
msg . error_status ) ;
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}
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# endif // AP_DRONECAN_HIMARK_SERVO_SUPPORT
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# if AP_DRONECAN_VOLZ_FEEDBACK_ENABLED
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void AP_DroneCAN : : handle_actuator_status_Volz ( const CanardRxTransfer & transfer , const com_volz_servo_ActuatorStatus & msg )
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{
AP : : logger ( ) . WriteStreaming (
" CVOL " ,
" TimeUS,Id,Pos,Cur,V,Pow,T " ,
" s#dAv%O " ,
" F-00000 " ,
" QBfffBh " ,
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AP_HAL : : micros64 ( ) ,
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msg . actuator_id ,
ToDeg ( msg . actual_position ) ,
msg . current * 0.025f ,
msg . voltage * 0.2f ,
msg . motor_pwm * ( 100.0 / 255.0 ) ,
int16_t ( msg . motor_temperature ) - 50 ) ;
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}
# endif
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/*
handle ESC status message
*/
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void AP_DroneCAN : : handle_ESC_status ( const CanardRxTransfer & transfer , const uavcan_equipment_esc_Status & msg )
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{
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# if HAL_WITH_ESC_TELEM
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const uint8_t esc_offset = constrain_int16 ( _esc_offset . get ( ) , 0 , DRONECAN_SRV_NUMBER ) ;
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const uint8_t esc_index = msg . esc_index + esc_offset ;
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if ( ! is_esc_data_index_valid ( esc_index ) ) {
return ;
}
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TelemetryData t {
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. temperature_cdeg = int16_t ( ( KELVIN_TO_C ( msg . temperature ) ) * 100 ) ,
. voltage = msg . voltage ,
. current = msg . current ,
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} ;
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update_rpm ( esc_index , msg . rpm , msg . error_count ) ;
update_telem_data ( esc_index , t ,
( isnan ( msg . current ) ? 0 : AP_ESC_Telem_Backend : : TelemetryType : : CURRENT )
| ( isnan ( msg . voltage ) ? 0 : AP_ESC_Telem_Backend : : TelemetryType : : VOLTAGE )
| ( isnan ( msg . temperature ) ? 0 : AP_ESC_Telem_Backend : : TelemetryType : : TEMPERATURE ) ) ;
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# endif
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}
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bool AP_DroneCAN : : is_esc_data_index_valid ( const uint8_t index ) {
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if ( index > DRONECAN_SRV_NUMBER ) {
// printf("DroneCAN: invalid esc index: %d. max index allowed: %d\n\r", index, DRONECAN_SRV_NUMBER);
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return false ;
}
return true ;
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}
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/*
handle LogMessage debug
*/
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void AP_DroneCAN : : handle_debug ( const CanardRxTransfer & transfer , const uavcan_protocol_debug_LogMessage & msg )
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{
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# if HAL_LOGGING_ENABLED
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if ( AP : : can ( ) . get_log_level ( ) ! = AP_CANManager : : LOG_NONE ) {
// log to onboard log and mavlink
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GCS_SEND_TEXT ( MAV_SEVERITY_INFO , " CAN[%u] %s " , transfer . source_node_id , msg . text . data ) ;
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} else {
// only log to onboard log
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AP : : logger ( ) . Write_MessageF ( " CAN[%u] %s " , transfer . source_node_id , msg . text . data ) ;
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}
# endif
}
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/*
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check for parameter get / set response timeout
*/
void AP_DroneCAN : : check_parameter_callback_timeout ( )
{
WITH_SEMAPHORE ( _param_sem ) ;
// return immediately if not waiting for get/set parameter response
if ( param_request_sent_ms = = 0 ) {
return ;
}
const uint32_t now_ms = AP_HAL : : millis ( ) ;
if ( now_ms - param_request_sent_ms > AP_DRONECAN_GETSET_TIMEOUT_MS ) {
param_request_sent_ms = 0 ;
param_int_cb = nullptr ;
param_float_cb = nullptr ;
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param_string_cb = nullptr ;
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}
}
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/*
send any queued request to get / set parameter
called from loop
*/
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void AP_DroneCAN : : send_parameter_request ( )
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{
WITH_SEMAPHORE ( _param_sem ) ;
if ( param_request_sent ) {
return ;
}
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param_get_set_client . request ( param_request_node_id , param_getset_req ) ;
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param_request_sent = true ;
}
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/*
set named float parameter on node
*/
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bool AP_DroneCAN : : set_parameter_on_node ( uint8_t node_id , const char * name , float value , ParamGetSetFloatCb * cb )
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{
WITH_SEMAPHORE ( _param_sem ) ;
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// fail if waiting for any previous get/set request
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if ( param_int_cb ! = nullptr | |
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param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
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return false ;
}
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param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) - 1 ) ;
param_getset_req . value . real_value = value ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_REAL_VALUE ;
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param_float_cb = cb ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = node_id ;
return true ;
}
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/*
set named integer parameter on node
*/
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bool AP_DroneCAN : : set_parameter_on_node ( uint8_t node_id , const char * name , int32_t value , ParamGetSetIntCb * cb )
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{
WITH_SEMAPHORE ( _param_sem ) ;
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// fail if waiting for any previous get/set request
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if ( param_int_cb ! = nullptr | |
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param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
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return false ;
}
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param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) - 1 ) ;
param_getset_req . value . integer_value = value ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_INTEGER_VALUE ;
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param_int_cb = cb ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = node_id ;
return true ;
}
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/*
set named string parameter on node
*/
bool AP_DroneCAN : : set_parameter_on_node ( uint8_t node_id , const char * name , const string & value , ParamGetSetStringCb * cb )
{
WITH_SEMAPHORE ( _param_sem ) ;
// fail if waiting for any previous get/set request
if ( param_int_cb ! = nullptr | |
param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
return false ;
}
param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) - 1 ) ;
memcpy ( & param_getset_req . value . string_value , ( const void * ) & value , sizeof ( value ) ) ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_STRING_VALUE ;
param_string_cb = cb ;
param_request_sent = false ;
param_request_sent_ms = AP_HAL : : millis ( ) ;
param_request_node_id = node_id ;
return true ;
}
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/*
get named float parameter on node
*/
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bool AP_DroneCAN : : get_parameter_on_node ( uint8_t node_id , const char * name , ParamGetSetFloatCb * cb )
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{
WITH_SEMAPHORE ( _param_sem ) ;
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// fail if waiting for any previous get/set request
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if ( param_int_cb ! = nullptr | |
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param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
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return false ;
}
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param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) ) ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_EMPTY ;
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param_float_cb = cb ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = node_id ;
return true ;
}
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/*
get named integer parameter on node
*/
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bool AP_DroneCAN : : get_parameter_on_node ( uint8_t node_id , const char * name , ParamGetSetIntCb * cb )
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{
WITH_SEMAPHORE ( _param_sem ) ;
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// fail if waiting for any previous get/set request
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if ( param_int_cb ! = nullptr | |
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param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
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return false ;
}
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param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) ) ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_EMPTY ;
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param_int_cb = cb ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = node_id ;
return true ;
}
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/*
get named string parameter on node
*/
bool AP_DroneCAN : : get_parameter_on_node ( uint8_t node_id , const char * name , ParamGetSetStringCb * cb )
{
WITH_SEMAPHORE ( _param_sem ) ;
// fail if waiting for any previous get/set request
if ( param_int_cb ! = nullptr | |
param_float_cb ! = nullptr | |
param_string_cb ! = nullptr ) {
return false ;
}
param_getset_req . index = 0 ;
param_getset_req . name . len = strncpy_noterm ( ( char * ) param_getset_req . name . data , name , sizeof ( param_getset_req . name . data ) ) ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_EMPTY ;
param_string_cb = cb ;
param_request_sent = false ;
param_request_sent_ms = AP_HAL : : millis ( ) ;
param_request_node_id = node_id ;
return true ;
}
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void AP_DroneCAN : : handle_param_get_set_response ( const CanardRxTransfer & transfer , const uavcan_protocol_param_GetSetResponse & rsp )
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{
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WITH_SEMAPHORE ( _param_sem ) ;
if ( ! param_int_cb & &
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! param_float_cb & &
! param_string_cb ) {
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return ;
}
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if ( ( rsp . value . union_tag = = UAVCAN_PROTOCOL_PARAM_VALUE_INTEGER_VALUE ) & & param_int_cb ) {
int32_t val = rsp . value . integer_value ;
if ( ( * param_int_cb ) ( this , transfer . source_node_id , ( const char * ) rsp . name . data , val ) ) {
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// we want the parameter to be set with val
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param_getset_req . index = 0 ;
memcpy ( param_getset_req . name . data , rsp . name . data , rsp . name . len ) ;
param_getset_req . value . integer_value = val ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_INTEGER_VALUE ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = transfer . source_node_id ;
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return ;
}
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} else if ( ( rsp . value . union_tag = = UAVCAN_PROTOCOL_PARAM_VALUE_REAL_VALUE ) & & param_float_cb ) {
float val = rsp . value . real_value ;
if ( ( * param_float_cb ) ( this , transfer . source_node_id , ( const char * ) rsp . name . data , val ) ) {
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// we want the parameter to be set with val
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param_getset_req . index = 0 ;
memcpy ( param_getset_req . name . data , rsp . name . data , rsp . name . len ) ;
param_getset_req . value . real_value = val ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_REAL_VALUE ;
param_request_sent = false ;
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param_request_sent_ms = AP_HAL : : millis ( ) ;
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param_request_node_id = transfer . source_node_id ;
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return ;
}
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} else if ( ( rsp . value . union_tag = = UAVCAN_PROTOCOL_PARAM_VALUE_STRING_VALUE ) & & param_string_cb ) {
string val ;
memcpy ( & val , & rsp . value . string_value , sizeof ( val ) ) ;
if ( ( * param_string_cb ) ( this , transfer . source_node_id , ( const char * ) rsp . name . data , val ) ) {
// we want the parameter to be set with val
param_getset_req . index = 0 ;
memcpy ( param_getset_req . name . data , rsp . name . data , rsp . name . len ) ;
memcpy ( & param_getset_req . value . string_value , & val , sizeof ( val ) ) ;
param_getset_req . value . union_tag = UAVCAN_PROTOCOL_PARAM_VALUE_STRING_VALUE ;
param_request_sent = false ;
param_request_sent_ms = AP_HAL : : millis ( ) ;
param_request_node_id = transfer . source_node_id ;
return ;
}
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}
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param_request_sent_ms = 0 ;
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param_int_cb = nullptr ;
param_float_cb = nullptr ;
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param_string_cb = nullptr ;
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}
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void AP_DroneCAN : : send_parameter_save_request ( )
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{
WITH_SEMAPHORE ( _param_save_sem ) ;
if ( param_save_request_sent ) {
return ;
}
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param_save_client . request ( param_save_request_node_id , param_save_req ) ;
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param_save_request_sent = true ;
}
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bool AP_DroneCAN : : save_parameters_on_node ( uint8_t node_id , ParamSaveCb * cb )
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{
WITH_SEMAPHORE ( _param_save_sem ) ;
if ( save_param_cb ! = nullptr ) {
//busy
return false ;
}
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param_save_req . opcode = UAVCAN_PROTOCOL_PARAM_EXECUTEOPCODE_REQUEST_OPCODE_SAVE ;
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param_save_request_sent = false ;
param_save_request_node_id = node_id ;
save_param_cb = cb ;
return true ;
}
// handle parameter save request response
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void AP_DroneCAN : : handle_param_save_response ( const CanardRxTransfer & transfer , const uavcan_protocol_param_ExecuteOpcodeResponse & rsp )
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{
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WITH_SEMAPHORE ( _param_save_sem ) ;
if ( ! save_param_cb ) {
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return ;
}
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( * save_param_cb ) ( this , transfer . source_node_id , rsp . ok ) ;
save_param_cb = nullptr ;
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}
// Send Reboot command
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// Note: Do not call this from outside DroneCAN thread context,
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// THIS IS NOT A THREAD SAFE API!
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void AP_DroneCAN : : send_reboot_request ( uint8_t node_id )
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{
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uavcan_protocol_RestartNodeRequest request ;
request . magic_number = UAVCAN_PROTOCOL_RESTARTNODE_REQUEST_MAGIC_NUMBER ;
restart_node_client . request ( node_id , request ) ;
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}
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// check if a option is set and if it is then reset it to 0.
// return true if it was set
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bool AP_DroneCAN : : check_and_reset_option ( Options option )
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{
bool ret = option_is_set ( option ) ;
if ( ret ) {
_options . set_and_save ( int16_t ( _options . get ( ) & ~ uint16_t ( option ) ) ) ;
}
return ret ;
}
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// handle prearm check
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bool AP_DroneCAN : : prearm_check ( char * fail_msg , uint8_t fail_msg_len ) const
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{
// forward this to DNA_Server
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return _dna_server . prearm_check ( fail_msg , fail_msg_len ) ;
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}
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/*
periodic logging
*/
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void AP_DroneCAN : : logging ( void )
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{
# if HAL_LOGGING_ENABLED
const uint32_t now_ms = AP_HAL : : millis ( ) ;
if ( now_ms - last_log_ms < 1000 ) {
return ;
}
last_log_ms = now_ms ;
if ( HAL_NUM_CAN_IFACES < = _driver_index ) {
// no interface?
return ;
}
const auto * iface = hal . can [ _driver_index ] ;
if ( iface = = nullptr ) {
return ;
}
const auto * stats = iface - > get_statistics ( ) ;
if ( stats = = nullptr ) {
// statistics not implemented on this interface
return ;
}
const auto & s = * stats ;
AP : : logger ( ) . WriteStreaming ( " CANS " ,
" TimeUS,I,T,Trq,Trej,Tov,Tto,Tab,R,Rov,Rer,Bo,Etx,Stx,Ftx " ,
" s#------------- " ,
" F-------------- " ,
" QBIIIIIIIIIIIII " ,
AP_HAL : : micros64 ( ) ,
_driver_index ,
s . tx_success ,
s . tx_requests ,
s . tx_rejected ,
s . tx_overflow ,
s . tx_timedout ,
s . tx_abort ,
s . rx_received ,
s . rx_overflow ,
s . rx_errors ,
s . num_busoff_err ,
_esc_send_count ,
_srv_send_count ,
_fail_send_count ) ;
# endif // HAL_LOGGING_ENABLED
}
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# endif // HAL_NUM_CAN_IFACES