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5383 Commits

Author SHA1 Message Date
svefro b473f8fd4d AP_RCMapper: Added warning to RCMAP_THROTTLE 
Warning user that changing RCMAP_Throttle could be dangerous
 2014-06-17 21:04:19 +10:00
Randy Mackay 9b81e46e61 AP_Common: add example sketch 2014-06-17 20:53:53 +10:00
Randy Mackay 2f7dee3ba5 AP_Mission: squeeze loiter turns radius into high byte of p1 2014-06-17 20:53:50 +10:00
Randy Mackay b79f729540 AP_Common: add LOWBYTE, HIGHBYTE macros 2014-06-17 20:53:47 +10:00
Randy Mackay fa16e0967f AP_Common: remove unused location mask definitions 2014-06-17 20:53:45 +10:00
Andrew Tridgell e2fe3d2de7 GCS_MAVLink: re-generate headers 2014-06-17 20:21:54 +10:00
Andrew Tridgell 0db226daf5 GCS_MAVLink: merge in upstream changes 2014-06-17 20:19:35 +10:00
Andrew Chapman 87fcfbf9dd GCS_MAVLink: re-generate MAVLink headers 2014-06-17 20:16:39 +10:00
Andrew Chapman 048767e389 GCS_MAVLink: camera feedback mavlink messages 
CAMERA_EVENT and CAMERA_FEEDBACK messages, and a couple of enums they
use (CAMERA_EVENT_TYPES and CAMERA_FEEDBACK_FLAGS)

Adjusted some types and added more explicit descriptions of units as
suggested on the call last week.

I will add camera parameter list/get/set functionality as suggested
using the existing parameter mechanism and component IDs rather than
the new CAMERA_INFO messages I had proposed.
 2014-06-17 20:15:20 +10:00
Randy Mackay 11e08e1492 DataFlash: common Log_Write_Camera 
pair programmed with Craig Elder
 2014-06-17 14:11:36 +10:00
Randy Mackay 0c9a496262 AC_AttControlHeli: add ATC_RATE_FF_ENAB parameter 
Because this class inherits from AC_AttitudeControl library this new
parameter must be added here as well
 2014-06-10 21:25:33 +09:00
Randy Mackay 46f25c52a4 AC_AttControl: allow enabling/disabling feedforward and accel limiting 2014-06-10 20:03:02 +09:00
Randy Mackay a2f54fdf2c AC_WPNav: smooth waypoint by freezing feed-forward and allowing overshoot 
First part of this fix is freezing the position controller's xy-axis
feed foward as we transition to the new segment.
Second part is work-around for straight line segments in that we allow
the target point to actually overshoot the end of the segment by up to
2m if the segment is a "fast waypoint".  Ideally we would instead notice
the waypoint has been completed and take any left over time or distance
and move our target along the track towards the next waypoint but that
would require a much larger change to allow the wpnav lib to hold the
next two waypoints.
 2014-06-10 20:03:01 +09:00
Randy Mackay ce85d1f6b2 AC_WPNav: use curr pos target as spline origin 
We only use the current target position as origin if the waypoint
controller is active (i..e has been used in the past 1 second).  This is
consistent with how we initialise straight line waypoints
 2014-06-10 20:02:59 +09:00
Randy Mackay 130eb07d48 AC_AttControl: angle_ef_roll_pitch_rate_ef_yaw supports zero yaw accel 2014-06-10 20:02:58 +09:00
Randy Mackay 02b4b21f67 AC_AttControl: disable feed forward by default 
Can be re-enabled by setting ATC_RATE_FF_ENAB parameter to 1
 2014-06-10 20:02:55 +09:00
Randy Mackay b57c0dabf6 AC_AttControl: check accel_rp_max instead of rate_bff_ff_enabled 
We use the accel_rp_max, accel_y_max to check whether to apply accel
limiting or not.  This is related to separate from the
body-frame-feed-forward.
 2014-06-10 20:02:54 +09:00
Randy Mackay 2bb30b3ef9 AC_AttControl: add set_yaw_target_to_current_heading method 2014-06-10 20:02:49 +09:00
Randy Mackay d9c966c927 AC_AttControl: RATE_FF_ENAB param to disable rate feed forward 2014-06-10 20:02:48 +09:00
Randy Mackay 4d4c7a2118 AC_AttControl: move freeze_ff to flags structure 2014-06-10 20:02:46 +09:00
Randy Mackay a662f87ffb AC_AttControl: remove resolved To-Do 
This To-Do is resolved by heli flight modes calling the
relax_bf_rate_controller method
 2014-06-10 20:02:45 +09:00
Randy Mackay 7f734f38d6 AC_AttControl: add earth frame angle constraints 
This should help recovery time if pilot switches out of ACRO (into
Stabilize, AltHold, etc) while inverted
 2014-06-10 20:02:43 +09:00
Randy Mackay 698cf934b8 AC_AttControl: formatting fixes 2014-06-10 20:02:42 +09:00
lthall 2bb63857fa AC_AttControl: clean up stabilize 2014-06-10 20:02:40 +09:00
lthall c24d293e1b AC_AttControl: zero _accel_xyz_max stops feed forward 
Also added place holder for turning off feed forward.
 2014-06-10 20:02:39 +09:00
lthall 8bbce7e658 AC_PosControl: freeze feed forward for alt control in Auto 2014-06-10 20:02:36 +09:00
lthall 922026c15c AC_AttControl: rate compensation for yaw 2014-06-10 20:02:34 +09:00
lthall 0d87298221 AC_PosControl: freeze feed forward and vector fixes 2014-06-10 20:02:33 +09:00
Randy Mackay 5209598459 AC_AttControl: rename init_targets to relax_bf_rate_controller 2014-06-10 20:02:27 +09:00
lthall 1bdde31f6b Copter: Fix zero throttle flip issue Stabilize 
The problem is that the init_targets is intended to ensure the
controller doesn't build up the I term when the throttle is low. Because
it is poorly named (or used) it have been written to do something else.
Here I change it to do what the code is trying to use it to do.
 2014-06-10 20:02:01 +09:00
Randy Mackay 915dad2da4 AC_Circle: use fast_atan2 to calc bearing from center 
This does not save much time because it's only called at initialisation
 2014-06-06 18:51:09 +09:00
Randy Mackay f23e94707c AC_WPNav: use fast_atan2 for bearing calcs 2014-06-06 18:51:08 +09:00
David Dewey 17374ff5e8 AP_Math: fast_atan2 
This is 126us per call vs 199us on the AVR.  it is accurate to about
0.28 degrees

Committed by rmackay9 but contribution is from David Dewey
 2014-06-06 18:50:41 +09:00
Ju1ien 28ce66f314 INav: clear historic z-axis position estimate when set_altitude called 2014-06-06 18:42:42 +09:00
Randy Mackay efd6d6dc70 AC_WPNav: spline div by zero fix 
Also add check for straight line navigation to ensure speed is not
reduced below zero when it hits the leash limit
Also minor formatting changes
 2014-06-05 22:23:38 +09:00
lthall 0912bec8f5 Spline div zero and leash limit fix 2014-06-05 22:23:35 +09:00
Andrew Tridgell f0df912a11 AP_Mission: added support for MAV_CMD_DO_INVERTED_FLIGHT 2014-06-05 15:44:18 +10:00
Andrew Tridgell ef4a79cc9a GCS_MAVLink: rebuild MAVLink headers 2014-06-05 15:44:03 +10:00
Andrew Tridgell 67937b5b79 GCS_MAVLink: added MAV_CMD_DO_INVERTED_FLIGHT 
used to invert from a mission
 2014-06-05 15:43:46 +10:00
Andrew Tridgell 5a1aa8dfe7 AP_L1_Control: implement turn_distance() with turn angle 
uses a linear approximation for now.
 2014-06-05 09:34:23 +10:00
Andrew Tridgell 7a6186f7e6 AP_Navigation: added a turn_distance() method with turn_angle 2014-06-05 09:33:42 +10:00
Andrew Tridgell 49f93b91b2 APM_OBC: fixed formatting to match APM coding standard 2014-06-02 10:47:02 +10:00
Andrew Tridgell e9e1799700 AP_Compass: fixed VRBrain build 2014-06-02 10:42:37 +10:00
Andrew Tridgell d554616e86 AP_EPM: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell 3705c90b8e AP_Baro: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell d70bee9249 AP_AHRS: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell 0d83d4f4f5 APM_OBC: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell 1e2214f8d1 DataFlash: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell 732cd0e130 AP_Relay: fix for HAL_GPIO_* 2014-06-02 10:42:36 +10:00
Andrew Tridgell 50c08ced4c AP_Notify: fixes for HAL_GPIO_* 2014-06-02 10:42:35 +10:00
Andrew Tridgell 4c43cd9775 AP_InertialSensor: fixes for HAL_GPIO_* 2014-06-02 10:42:35 +10:00
Andrew Tridgell 805d79debe HAL_FLYMAPLE: fix for HAL_GPIO_* 2014-06-02 10:42:35 +10:00
Andrew Tridgell 3015356671 HAL_AVR: fixes for HAL_GPIO_ define change 2014-06-02 10:42:35 +10:00
Andrew Tridgell 18a64d17d3 AP_HAL: added HAL_ prefix to GPIO_ defines 
this fixes a bug caused by GPIO_INPUT and GPIO_OUTPUT already being
defined in NuttX, which caused pinMode() not to setup pins for output
when requested
 2014-06-02 09:24:52 +10:00
Andrew Tridgell fa4eb5475a HAL_PX4: implement analog input stop pins 
this allows multiple sonars to cooperate without interference
 2014-06-02 08:35:41 +10:00
Randy Mackay 2b0f142a17 AC_PosControl: fix typo in D-filter definition 2014-05-29 17:50:48 +09:00
Randy Mackay 7e3213edbf AC_AttControl: increase default accel max 2014-05-29 17:40:26 +09:00
Randy Mackay 29ca7a10df AC_PosControl: set alt hold accel control D term filter 2014-05-29 17:40:23 +09:00
Randy Mackay 0969e464fb AC_AttControl: set roll, pitch, yaw rate control D term filters 2014-05-29 17:40:17 +09:00
Randy Mackay faf3415e5e AC_PID: example sketch prints individual P, I and D values 2014-05-29 17:39:19 +09:00
Robert Lefebvre b35ec4339e AC_PID: Add method to set the D-term Filter Rate from main code. 2014-05-29 17:39:10 +09:00
Robert Lefebvre f1c3f2a3d1 AC_PID: Remove get_leaky_i function which is now found in AC_HELI_PID. 2014-05-29 17:39:08 +09:00
Robert Lefebvre 7c9249de93 AC_AttitudeControl_Heli: Change to use AC_HELI_PID class instead of AC_PID. Remove FF parameters from class. 2014-05-29 17:39:06 +09:00
Robert Lefebvre 6333b4bba6 AC_PID: update example sketch to test AC_HELI_PID 2014-05-29 17:39:01 +09:00
Robert Lefebvre ef7dc815cd AC_PID: Change Private members to Protected so that AC_HELI_PID can access them. 2014-05-29 17:38:59 +09:00
Robert Lefebvre 94e9bed9cf AC_PID: Add new AC_HELI_PID as a child of AC_PID 2014-05-29 17:38:57 +09:00
Andrew Tridgell 0b6407256c GCS_MAVLink: moved 3 more send_*() functions to GCS_Common.cpp 2014-05-28 09:35:30 +10:00
Andrew Tridgell 37c50d9587 HAL_PX4: fixed use of FMU servo pins as digital inputs 
these pins can be PWM output or digital input or digital output
 2014-05-25 22:03:44 +10:00
Andrew Tridgell 2d9e9d9bc3 AP_Compass: added COMPASS_PRIMARY parameter 
this allows selection of which compass is the primary. Useful if the
first compass starts giving spurious data (as happened in our plane)
 2014-05-25 22:03:44 +10:00
priseborough edc79ca2a4 AP_NavEKF: Increase divergence test margin based on analysis of more user flight logs 
Analysis of copter logs has shown cases with a healthy EKF where spikes in EKF4.DS of up to 25% of the threshold have occurred.
A value of closer to 10% for normal operation is preferred.
 2014-05-24 22:20:24 +10:00
Andrew Tridgell aba11a0634 AP_L1_Control: wrap the target_bearing 2014-05-23 07:30:58 +10:00
Randy Mackay cde7d31dad AC_WPNav: fix divide by zero when origin and dest are same location 2014-05-22 21:18:24 +09:00
Andrew Tridgell 63da53c842 GCS_MAVLink: moved main update() routine into GCS_Common.cpp 
this fixes a common timeout error with loading large missions, and
means less per-vehicle code
 2014-05-21 12:45:25 +10:00
Andrew Tridgell 42c1501563 AP_Common: moved map_baudrate() into AP_Common 
this version supports a much wider range of baudrates
 2014-05-21 12:45:25 +10:00
Andrew Tridgell 7d712f90bf APM_OBC: adjusted docs for FS_HB_PIN 
thanks to Warren for the question
 2014-05-21 12:45:25 +10:00
Randy Mackay 69ad632e2a GPS: correct NAVFILTER parameter description 
These corrected values match the GPS_Engine_Setting enum in GPS.h
Thanks to Adolfo R for noticing the issue and providing the fix
 2014-05-20 22:08:40 +09:00
Andrew Tridgell a7d6a26bec HAL_PX4: fixed auto-flow control 
the 6 bytes written to break the radio out of bootloader broke
auto flowcontrol detection
 2014-05-19 22:02:39 +10:00
Randy Mackay 597d5227f5 AC_WPNav: rename set_loiter_target to init_loiter_target 2014-05-19 12:27:25 +09:00
Randy Mackay e7b3c00767 AC_WPNav: set_loiter_target uses set_xy_target 
Loiter is only a horizontal position controller so it should not set the
z-axis position.
Moved pos_control.set_speed and accel functions so order matches
init_loiter_targets function order
 2014-05-19 12:27:20 +09:00
Ju1ien aed5787c1b AC_WPNav: bug fix for loiter init in Hybrid 
AC_PosControl::init_xy_controller() has been added to PosControl and is
called by init_loiter_target.
Hybrid is currently using set_loiter_target function to init the loiter
controller. So we have to call init_xy_controller() by set_loiter_target
function.
What happens otherwise?
In AC_PosControl::update_xy_controller, we update "now" with
now = hal.scheduler->millis();
and, as _last_update_xy_ms has not been updated previously by
init_xy_controller(), we just call init_xy_controller().
So, _dt_xy  will be negative and used anyways in all the functions and
PID called by update_xy_controller.
That will avoid at least _accel_target.x/y to be set to 0 but I'm not
sure for the high values, probably an I_term that is not reset and
reached very high value.
Or maybe a cast error somewhere... no clue at all
 2014-05-19 12:27:16 +09:00
priseborough 5fe0d2c1b2 AP_NavEKF: Add protection for accel bias estimation errors 
Don't do bias estimation if tilted by more than 60 degrees to prevent scale
factor errors affecting result unnecessarily.
Prevent Kalman gain from having the wrong sign due to numerical errors
associated with small process noise values.
Allow smaller Z accel bias process noise values to be set
 2014-05-18 08:09:00 +10:00
priseborough 3222e8f7cb AP_NavEKF: Default parameter adjustments 
Bring Plane glitch protection thresholds into alignment with copter and
rover
Slight increase in accelerometer bias process noise to prevent bias
estimate divergence into limits (Rover and Plane only as Copter does not
seem respond as well to this change)
effective increase in threshold on divergence test to allow increased
margin for bad GPS velocities
 2014-05-18 08:08:49 +10:00
Andrew Tridgell 65fd25fb5a AP_InertialSensor: fixed example build 2014-05-18 08:08:19 +10:00
Andrew Tridgell b99ae63cbb HAL_Linux: more generic fix for scheduler issues in example sketches 
this ensures drivers can run
 2014-05-16 22:40:38 +10:00
Andrew Tridgell 30f5e2c37f AP_GPS: work around scheduling issue in example code 2014-05-16 22:35:32 +10:00
priseborough e40e50e2e1 AP_NavEKF: Prevent start-up transients re-tripping divergence test 2014-05-16 22:05:22 +10:00
Andrew Tridgell 73976e2ca4 AP_GPS: fixed example build 2014-05-16 22:05:04 +10:00
Andrew Tridgell 8533aecf18 AP_InertialSensor: fixed example build 2014-05-16 21:24:25 +10:00
priseborough a19015ed61 AP_NavEKF: Scale divergence check with covariance 
This provides consistent behaviour for a range of gyro bias process
noise settings and automatically adjusts sensitivity as filter learns bias
 2014-05-16 21:24:25 +10:00
priseborough 0337d44b2e AP_NavEKF: Fix bug causing immediate clearing of diverged status on reset 2014-05-16 21:24:04 +10:00
priseborough d150904dc6 AP_NavEKF: Increase gyro bias process noise 
This is required to stop the bias estimate from becoming too static
towards the end of longer flights.
 2014-05-16 21:24:04 +10:00
Andrew Tridgell 49e7ee9ba7 GCS_MAVLink: added setup_uart() method 
this provides a common way of dealing with UART setup for a GCS
instance. It includes code to cope with SiK radios stuck in bootloader
mode.
 2014-05-16 11:44:33 +10:00
Andrew Tridgell b3c1e515dc AP_AHRS: when no accel info available in buffer use current value 
this prevents an initialisation error, and is reasonable in flight too

Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>
 2014-05-15 22:19:54 +10:00
Andrew Tridgell 315290029a AP_AHRS: fixed check of accel sensor health 
we need to check health of each accelerometer separately
 2014-05-15 22:18:56 +10:00
Andrew Tridgell 5edf4ba596 AP_NavEKF: fixed up handling of bitfields in faultStatus 
Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>
 2014-05-15 21:42:39 +10:00
Andrew Tridgell 79edc4b467 GCS_MAVLink: re-generate with addition of MAV_SYS_STATUS_AHRS 2014-05-15 21:14:21 +10:00
Andrew Tridgell ccebeba5a5 GCS_MAVLink: added MAV_SYS_STATUS_AHRS 
will be used to indicate AHRS health
 2014-05-15 21:14:21 +10:00
priseborough f01cc78d37 DataFlash: Add EKF fault status logging 2014-05-15 21:14:21 +10:00
priseborough ce8e1daa16 AP_NavEKF: Improved divergence detection and reset 
Divergence is now detected by looking for very large changes in the gyro
bias. This will cause the filter to be reset and declared unhealthy for
10 seconds.

Don't reset filterDiverged status immediately during reset

Set filterDiverged true if covariance blows up

Add fault status reporting
 2014-05-15 21:14:21 +10:00
Andrew Tridgell 5d2d6e0063 GCS_MAVLink: regenerated MAVLink headers 2014-05-15 21:14:21 +10:00