mirror of https://github.com/ArduPilot/ardupilot
417 lines
18 KiB
C++
417 lines
18 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
|
|
/*
|
|
This program 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.
|
|
|
|
This program 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/>.
|
|
*/
|
|
|
|
/*
|
|
APM_OBC.cpp
|
|
|
|
Outback Challenge Failsafe module
|
|
|
|
*/
|
|
#include <AP_HAL/AP_HAL.h>
|
|
#include "APM_OBC.h"
|
|
#include <RC_Channel/RC_Channel.h>
|
|
#include <RC_Channel/RC_Channel_aux.h>
|
|
#include <GCS_MAVLink/GCS.h>
|
|
|
|
extern const AP_HAL::HAL& hal;
|
|
|
|
// table of user settable parameters
|
|
const AP_Param::GroupInfo APM_OBC::var_info[] = {
|
|
// @Param: MAN_PIN
|
|
// @DisplayName: Manual Pin
|
|
// @Description: This sets a digital output pin to set high when in manual mode
|
|
// @User: Advanced
|
|
AP_GROUPINFO("MAN_PIN", 0, APM_OBC, _manual_pin, -1),
|
|
|
|
// @Param: HB_PIN
|
|
// @DisplayName: Heartbeat Pin
|
|
// @Description: This sets a digital output pin which is cycled at 10Hz when termination is not activated. Note that if a FS_TERM_PIN is set then the heartbeat pin will continue to cycle at 10Hz when termination is activated, to allow the termination board to distinguish between autopilot crash and termination.
|
|
// @User: Advanced
|
|
AP_GROUPINFO("HB_PIN", 1, APM_OBC, _heartbeat_pin, -1),
|
|
|
|
// @Param: WP_COMMS
|
|
// @DisplayName: Comms Waypoint
|
|
// @Description: Waypoint number to navigate to on comms loss
|
|
// @User: Advanced
|
|
AP_GROUPINFO("WP_COMMS", 2, APM_OBC, _wp_comms_hold, 0),
|
|
|
|
// @Param: GPS_LOSS
|
|
// @DisplayName: GPS Loss Waypoint
|
|
// @Description: Waypoint number to navigate to on GPS lock loss
|
|
// @User: Advanced
|
|
AP_GROUPINFO("WP_GPS_LOSS", 4, APM_OBC, _wp_gps_loss, 0),
|
|
|
|
// @Param: TERMINATE
|
|
// @DisplayName: Force Terminate
|
|
// @Description: Can be set in flight to force termination of the heartbeat signal
|
|
// @User: Advanced
|
|
AP_GROUPINFO("TERMINATE", 5, APM_OBC, _terminate, 0),
|
|
|
|
// @Param: TERM_ACTION
|
|
// @DisplayName: Terminate action
|
|
// @Description: This can be used to force an action on flight termination. Normally this is handled by an external failsafe board, but you can setup APM to handle it here. If set to 0 (which is the default) then no extra action is taken. If set to the magic value 42 then the plane will deliberately crash itself by setting maximum throws on all surfaces, and zero throttle
|
|
// @User: Advanced
|
|
AP_GROUPINFO("TERM_ACTION", 6, APM_OBC, _terminate_action, 0),
|
|
|
|
// @Param: TERM_PIN
|
|
// @DisplayName: Terminate Pin
|
|
// @Description: This sets a digital output pin to set high on flight termination
|
|
// @User: Advanced
|
|
AP_GROUPINFO("TERM_PIN", 7, APM_OBC, _terminate_pin, -1),
|
|
|
|
// @Param: AMSL_LIMIT
|
|
// @DisplayName: AMSL limit
|
|
// @Description: This sets the AMSL (above mean sea level) altitude limit. If the pressure altitude determined by QNH exceeds this limit then flight termination will be forced. Note that this limit is in meters, whereas pressure altitude limits are often quoted in feet. A value of zero disables the pressure altitude limit.
|
|
// @User: Advanced
|
|
// @Units: meters
|
|
AP_GROUPINFO("AMSL_LIMIT", 8, APM_OBC, _amsl_limit, 0),
|
|
|
|
// @Param: AMSL_ERR_GPS
|
|
// @DisplayName: Error margin for GPS based AMSL limit
|
|
// @Description: This sets margin for error in GPS derived altitude limit. This error margin is only used if the barometer has failed. If the barometer fails then the GPS will be used to enforce the AMSL_LIMIT, but this margin will be subtracted from the AMSL_LIMIT first, to ensure that even with the given amount of GPS altitude error the pressure altitude is not breached. OBC users should set this to comply with their D2 safety case. A value of -1 will mean that barometer failure will lead to immediate termination.
|
|
// @User: Advanced
|
|
// @Units: meters
|
|
AP_GROUPINFO("AMSL_ERR_GPS", 9, APM_OBC, _amsl_margin_gps, -1),
|
|
|
|
// @Param: QNH_PRESSURE
|
|
// @DisplayName: QNH pressure
|
|
// @Description: This sets the QNH pressure in millibars to be used for pressure altitude in the altitude limit. A value of zero disables the altitude limit.
|
|
// @Units: millibar
|
|
// @User: Advanced
|
|
AP_GROUPINFO("QNH_PRESSURE", 10, APM_OBC, _qnh_pressure, 0),
|
|
|
|
// @Param: ENABLE
|
|
// @DisplayName: Enable Advanced Failsafe
|
|
// @Description: This enables the advanced failsafe system. If this is set to zero (disable) then all the other AFS options have no effect
|
|
// @User: Advanced
|
|
AP_GROUPINFO("ENABLE", 11, APM_OBC, _enable, 0),
|
|
|
|
// *NOTE* index 12 of AP_Int16 RC_FAIL_MS was depreciated. Replaced by RC_FAIL_TIME.
|
|
|
|
// @Param: MAX_GPS_LOSS
|
|
// @DisplayName: Maximum number of GPS loss events
|
|
// @Description: Maximum number of GPS loss events before the aircraft stops returning to mission on GPS recovery. Use zero to allow for any number of GPS loss events.
|
|
// @User: Advanced
|
|
AP_GROUPINFO("MAX_GPS_LOSS", 13, APM_OBC, _max_gps_loss, 0),
|
|
|
|
// @Param: MAX_COM_LOSS
|
|
// @DisplayName: Maximum number of comms loss events
|
|
// @Description: Maximum number of comms loss events before the aircraft stops returning to mission on comms recovery. Use zero to allow for any number of comms loss events.
|
|
// @User: Advanced
|
|
AP_GROUPINFO("MAX_COM_LOSS", 14, APM_OBC, _max_comms_loss, 0),
|
|
|
|
// @Param: GEOFENCE
|
|
// @DisplayName: Enable geofence Advanced Failsafe
|
|
// @Description: This enables the geofence part of the AFS. Will only be in effect if AFS_ENABLE is also 1
|
|
// @User: Advanced
|
|
AP_GROUPINFO("GEOFENCE", 15, APM_OBC, _enable_geofence_fs, 1),
|
|
|
|
// @Param: RC
|
|
// @DisplayName: Enable RC Advanced Failsafe
|
|
// @Description: This enables the RC part of the AFS. Will only be in effect if AFS_ENABLE is also 1
|
|
// @User: Advanced
|
|
AP_GROUPINFO("RC", 16, APM_OBC, _enable_RC_fs, 1),
|
|
|
|
// @Param: RC_MAN_ONLY
|
|
// @DisplayName: Enable RC Termination only in manual control modes
|
|
// @Description: If this parameter is set to 1, then an RC loss will only cause the plane to terminate in manual control modes. If it is 0, then the plane will terminate in any flight mode.
|
|
// @User: Advanced
|
|
AP_GROUPINFO("RC_MAN_ONLY", 17, APM_OBC, _rc_term_manual_only, 1),
|
|
|
|
// @Param: DUAL_LOSS
|
|
// @DisplayName: Enable dual loss terminate due to failure of both GCS and GPS simultaneously
|
|
// @Description: This enables the dual loss termination part of the AFS system. If this parameter is 1 and both GPS and the ground control station fail simultaneously, this will be considered a "dual loss" and cause termination.
|
|
// @User: Advanced
|
|
AP_GROUPINFO("DUAL_LOSS", 18, APM_OBC, _enable_dual_loss, 1),
|
|
|
|
// @Param: RC_FAIL_TIME
|
|
// @DisplayName: RC failure time
|
|
// @Description: This is the time in seconds in manual mode that failsafe termination will activate if RC input is lost. For the OBC rules this should be (1.5). Use 0 to disable.
|
|
// @User: Advanced
|
|
// @Units: seconds
|
|
AP_GROUPINFO("RC_FAIL_TIME", 19, APM_OBC, _rc_fail_time_seconds, 0),
|
|
|
|
AP_GROUPEND
|
|
};
|
|
|
|
// check for Failsafe conditions. This is called at 10Hz by the main
|
|
// ArduPlane code
|
|
void
|
|
APM_OBC::check(APM_OBC::control_mode mode, uint32_t last_heartbeat_ms, bool geofence_breached, uint32_t last_valid_rc_ms)
|
|
{
|
|
if (!_enable) {
|
|
return;
|
|
}
|
|
// we always check for fence breach
|
|
if(_enable_geofence_fs) {
|
|
if (geofence_breached || check_altlimit()) {
|
|
if (!_terminate) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "Fence TERMINATE");
|
|
_terminate.set(1);
|
|
}
|
|
}
|
|
}
|
|
|
|
// check if RC termination is enabled
|
|
// check for RC failure in manual mode or RC failure when AFS_RC_MANUAL is 0
|
|
if (_state != STATE_PREFLIGHT && !_terminate && _enable_RC_fs &&
|
|
(mode == OBC_MANUAL || mode == OBC_FBW || !_rc_term_manual_only) &&
|
|
_rc_fail_time_seconds > 0 &&
|
|
(AP_HAL::millis() - last_valid_rc_ms) > (_rc_fail_time_seconds * 1000.0f)) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "RC failure terminate");
|
|
_terminate.set(1);
|
|
}
|
|
|
|
// tell the failsafe board if we are in manual control
|
|
// mode. This tells it to pass through controls from the
|
|
// receiver
|
|
if (_manual_pin != -1) {
|
|
hal.gpio->pinMode(_manual_pin, HAL_GPIO_OUTPUT);
|
|
hal.gpio->write(_manual_pin, mode==OBC_MANUAL);
|
|
}
|
|
|
|
uint32_t now = AP_HAL::millis();
|
|
bool gcs_link_ok = ((now - last_heartbeat_ms) < 10000);
|
|
bool gps_lock_ok = ((now - gps.last_fix_time_ms()) < 3000);
|
|
|
|
switch (_state) {
|
|
case STATE_PREFLIGHT:
|
|
// we startup in preflight mode. This mode ends when
|
|
// we first enter auto.
|
|
if (mode == OBC_AUTO) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "Starting AFS_AUTO");
|
|
_state = STATE_AUTO;
|
|
}
|
|
break;
|
|
|
|
case STATE_AUTO:
|
|
// this is the normal mode.
|
|
if (!gcs_link_ok) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_ERROR, "State DATA_LINK_LOSS");
|
|
_state = STATE_DATA_LINK_LOSS;
|
|
if (_wp_comms_hold) {
|
|
_saved_wp = mission.get_current_nav_cmd().index;
|
|
mission.set_current_cmd(_wp_comms_hold);
|
|
}
|
|
// if two events happen within 30s we consider it to be part of the same event
|
|
if (now - _last_comms_loss_ms > 30*1000UL) {
|
|
_comms_loss_count++;
|
|
_last_comms_loss_ms = now;
|
|
}
|
|
break;
|
|
}
|
|
if (!gps_lock_ok) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "State GPS_LOSS");
|
|
_state = STATE_GPS_LOSS;
|
|
if (_wp_gps_loss) {
|
|
_saved_wp = mission.get_current_nav_cmd().index;
|
|
mission.set_current_cmd(_wp_gps_loss);
|
|
}
|
|
// if two events happen within 30s we consider it to be part of the same event
|
|
if (now - _last_gps_loss_ms > 30*1000UL) {
|
|
_gps_loss_count++;
|
|
_last_gps_loss_ms = now;
|
|
}
|
|
break;
|
|
}
|
|
break;
|
|
|
|
case STATE_DATA_LINK_LOSS:
|
|
if (!gps_lock_ok) {
|
|
// losing GPS lock when data link is lost
|
|
// leads to termination if AFS_DUAL_LOSS is 1
|
|
if(_enable_dual_loss) {
|
|
if (!_terminate) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "Dual loss TERMINATE");
|
|
_terminate.set(1);
|
|
}
|
|
}
|
|
} else if (gcs_link_ok) {
|
|
_state = STATE_AUTO;
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "GCS OK");
|
|
// we only return to the mission if we have not exceeded AFS_MAX_COM_LOSS
|
|
if (_saved_wp != 0 &&
|
|
(_max_comms_loss <= 0 ||
|
|
_comms_loss_count <= _max_comms_loss)) {
|
|
mission.set_current_cmd(_saved_wp);
|
|
_saved_wp = 0;
|
|
}
|
|
}
|
|
break;
|
|
|
|
case STATE_GPS_LOSS:
|
|
if (!gcs_link_ok) {
|
|
// losing GCS link when GPS lock lost
|
|
// leads to termination if AFS_DUAL_LOSS is 1
|
|
if (!_terminate && _enable_dual_loss) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "Dual loss TERMINATE");
|
|
_terminate.set(1);
|
|
}
|
|
} else if (gps_lock_ok) {
|
|
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_INFO, "GPS OK");
|
|
_state = STATE_AUTO;
|
|
// we only return to the mission if we have not exceeded AFS_MAX_GPS_LOSS
|
|
if (_saved_wp != 0 &&
|
|
(_max_gps_loss <= 0 || _gps_loss_count <= _max_gps_loss)) {
|
|
mission.set_current_cmd(_saved_wp);
|
|
_saved_wp = 0;
|
|
}
|
|
}
|
|
break;
|
|
}
|
|
|
|
// if we are not terminating or if there is a separate terminate
|
|
// pin configured then toggle the heartbeat pin at 10Hz
|
|
if (_heartbeat_pin != -1 && (_terminate_pin != -1 || !_terminate)) {
|
|
_heartbeat_pin_value = !_heartbeat_pin_value;
|
|
hal.gpio->pinMode(_heartbeat_pin, HAL_GPIO_OUTPUT);
|
|
hal.gpio->write(_heartbeat_pin, _heartbeat_pin_value);
|
|
}
|
|
|
|
// set the terminate pin
|
|
if (_terminate_pin != -1) {
|
|
hal.gpio->pinMode(_terminate_pin, HAL_GPIO_OUTPUT);
|
|
hal.gpio->write(_terminate_pin, _terminate?1:0);
|
|
}
|
|
}
|
|
|
|
|
|
// send heartbeat messages during sensor calibration
|
|
void
|
|
APM_OBC::heartbeat(void)
|
|
{
|
|
if (!_enable) {
|
|
return;
|
|
}
|
|
|
|
// if we are not terminating or if there is a separate terminate
|
|
// pin configured then toggle the heartbeat pin at 10Hz
|
|
if (_heartbeat_pin != -1 && (_terminate_pin != -1 || !_terminate)) {
|
|
_heartbeat_pin_value = !_heartbeat_pin_value;
|
|
hal.gpio->pinMode(_heartbeat_pin, HAL_GPIO_OUTPUT);
|
|
hal.gpio->write(_heartbeat_pin, _heartbeat_pin_value);
|
|
}
|
|
}
|
|
|
|
// check for altitude limit breach
|
|
bool
|
|
APM_OBC::check_altlimit(void)
|
|
{
|
|
if (!_enable) {
|
|
return false;
|
|
}
|
|
if (_amsl_limit == 0 || _qnh_pressure <= 0) {
|
|
// no limit set
|
|
return false;
|
|
}
|
|
|
|
// see if the barometer is dead
|
|
if (AP_HAL::millis() - baro.get_last_update() > 5000) {
|
|
// the barometer has been unresponsive for 5 seconds. See if we can switch to GPS
|
|
if (_amsl_margin_gps != -1 &&
|
|
gps.status() >= AP_GPS::GPS_OK_FIX_3D &&
|
|
gps.location().alt*0.01f <= _amsl_limit - _amsl_margin_gps) {
|
|
// GPS based altitude OK
|
|
return false;
|
|
}
|
|
// no barometer - immediate termination
|
|
return true;
|
|
}
|
|
|
|
float alt_amsl = baro.get_altitude_difference(_qnh_pressure*100, baro.get_pressure());
|
|
if (alt_amsl > _amsl_limit) {
|
|
// pressure altitude breach
|
|
return true;
|
|
}
|
|
|
|
// all OK
|
|
return false;
|
|
}
|
|
|
|
/*
|
|
setup the IO boards failsafe values for if the FMU firmware crashes
|
|
*/
|
|
void APM_OBC::setup_failsafe(void)
|
|
{
|
|
if (!_enable) {
|
|
return;
|
|
}
|
|
const RC_Channel *ch_roll = RC_Channel::rc_channel(rcmap.roll()-1);
|
|
const RC_Channel *ch_pitch = RC_Channel::rc_channel(rcmap.pitch()-1);
|
|
const RC_Channel *ch_yaw = RC_Channel::rc_channel(rcmap.yaw()-1);
|
|
const RC_Channel *ch_throttle = RC_Channel::rc_channel(rcmap.throttle()-1);
|
|
|
|
// setup primary channel output values
|
|
hal.rcout->set_failsafe_pwm(1U<<(rcmap.roll()-1), ch_roll->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MIN));
|
|
hal.rcout->set_failsafe_pwm(1U<<(rcmap.pitch()-1), ch_pitch->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MAX));
|
|
hal.rcout->set_failsafe_pwm(1U<<(rcmap.yaw()-1), ch_yaw->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MAX));
|
|
hal.rcout->set_failsafe_pwm(1U<<(rcmap.throttle()-1), ch_throttle->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MIN));
|
|
|
|
// and all aux channels
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_flap_auto, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_flap, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_aileron, RC_Channel::RC_CHANNEL_LIMIT_MIN);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_rudder, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_elevator, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_elevator_with_input, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_manual, RC_Channel::RC_CHANNEL_LIMIT_TRIM);
|
|
RC_Channel_aux::set_servo_failsafe(RC_Channel_aux::k_none, RC_Channel::RC_CHANNEL_LIMIT_TRIM);
|
|
}
|
|
|
|
/*
|
|
setu radio_out values for all channels to termination values if we
|
|
are terminating
|
|
*/
|
|
void APM_OBC::check_crash_plane(void)
|
|
{
|
|
if (!_enable) {
|
|
return;
|
|
}
|
|
// ensure failsafe values are setup for if FMU crashes on PX4/Pixhawk
|
|
if (!_failsafe_setup) {
|
|
_failsafe_setup = true;
|
|
setup_failsafe();
|
|
}
|
|
|
|
// should we crash the plane? Only possible with
|
|
// FS_TERM_ACTTION set to 42
|
|
if (!_terminate || _terminate_action != 42) {
|
|
// not terminating
|
|
return;
|
|
}
|
|
|
|
// we are terminating. Setup primary output channels radio_out values
|
|
RC_Channel *ch_roll = RC_Channel::rc_channel(rcmap.roll()-1);
|
|
RC_Channel *ch_pitch = RC_Channel::rc_channel(rcmap.pitch()-1);
|
|
RC_Channel *ch_yaw = RC_Channel::rc_channel(rcmap.yaw()-1);
|
|
RC_Channel *ch_throttle = RC_Channel::rc_channel(rcmap.throttle()-1);
|
|
|
|
ch_roll->set_radio_out(ch_roll->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MIN));
|
|
ch_pitch->set_radio_out(ch_pitch->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MAX));
|
|
ch_yaw->set_radio_out(ch_yaw->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MAX));
|
|
ch_throttle->set_radio_out(ch_throttle->get_limit_pwm(RC_Channel::RC_CHANNEL_LIMIT_MIN));
|
|
|
|
// and all aux channels
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_flap_auto, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_flap, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_aileron, RC_Channel::RC_CHANNEL_LIMIT_MIN);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_rudder, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_elevator, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_elevator_with_input, RC_Channel::RC_CHANNEL_LIMIT_MAX);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_manual, RC_Channel::RC_CHANNEL_LIMIT_TRIM);
|
|
RC_Channel_aux::set_servo_limit(RC_Channel_aux::k_none, RC_Channel::RC_CHANNEL_LIMIT_TRIM);
|
|
}
|