d7e4310df0
DataFlash: Lat can be negative in POS
10 years ago
559684b257
GCS_MAVLink: fix flow control check
...
Thanks to Tridge for spotting is
10 years ago
b0a90df135
DataFlash: fixed double Init of DF object
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thanks to Michael De Breuil
10 years ago
763c671d0a
GCS_Console: fix example sketch after mavlink_comm_port to array
10 years ago
85eeba93c0
GCS_MAVLink: mavlink_comm_port to array
10 years ago
facbfaf31f
SerialManager: support for 4th mavlink channel
10 years ago
62e7e8cc7d
GCS_MAVLink: add support for 4th mavlink chan on PX4
10 years ago
74485c5754
DataFlash: added Log_Write_POS() call
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write AHRS position to DF log
10 years ago
3370ec62a1
HAL_SITL: fix for multi-compass SITL
10 years ago
91b4ba3588
AP_Compass: allow for more than one compass in HIL/SITL
10 years ago
11f70da8b4
DataFlash: fixed incorrect change to GPS message
10 years ago
ade4f81c77
Compass: fix example sketch
10 years ago
bd91b9727f
AP_NavEKF: Add pre-arm check for horizontal inertial errors
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This check will declare the EKF as unhealthy if the horizontal position innovations exceed a threshold before motors are armed.
This will help to prevent a takeoff with bad inertial data caused by bad accel or gyro offsets.
10 years ago
1b13250fd8
RC_Channel: small parameter description change
10 years ago
61c851885f
AC_WPNav: remove unused set_spline_dest_and_vel
10 years ago
7056484ef0
Copter: fix spline overshoot
10 years ago
56b92e7d8c
AC_PID: fix example sketch
10 years ago
c2ac80cc63
AP_AHRS: Prevent copter from switching to DCM unless EKF has severe errors
10 years ago
3f8b832075
InertialSensor: fix example sketch
10 years ago
3bcd97fcd1
Parachute: increase deployment duration to 2sec
10 years ago
5560d3dba1
BattMonitor: fix example sketch
10 years ago
e080b2acce
AP_Arming: use accel_calibrated_ok_all
10 years ago
1f14eec4ea
InertialSensor: accel_calibrated_all_ok replaces calibrated
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This checks that the current number of accelerometers matches the number
of calibrated accels in order to catch accel failures at boot
10 years ago
0d72f3ac29
AP_HAL: fix example sketches
10 years ago
8bf2baef70
AP_InertialSensor: fixed primary accel/gyro in replay
10 years ago
f40c96de9d
SITL: add 'quad' and 'copter' as aliases for quadcopter
10 years ago
2a47cc3c81
HAL_SITL: cleanup command line handling
10 years ago
bab94c8a04
SITL: close high fds before launching JSBSIM
10 years ago
414f4125de
AP_HAL: use FD_CLOEXEC to prevent sockets being inherited in SITL
10 years ago
7692889248
SIM_JSBSim: added elevon and vtail support
10 years ago
aa9853179c
SITL: fixed startup yaw
10 years ago
5687adbdba
HAL_SITL: support JSBSim backend
10 years ago
692fc18698
AP_HAL: protect Socket.h from double include
10 years ago
c136d65c25
SITL: added initial JSBSim simulator backend
10 years ago
8ec98a5ec9
SITL: make it possible to connect two SITL instances together
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this adds --client to set uartC as a tcp client rather than a TCP
server
10 years ago
3991e0c476
DataFlash: fixed sign of sv in GRAW message
10 years ago
3529e02675
AP_AHRS: if we have 3 gyros then only use first two
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the 3rd gyro on a PH2 has a lot more noise as it is not vibration
isolated
10 years ago
cb59570938
AP_NavEKF: Remove bug preventing external selection of optical flow mode
10 years ago
3390d9932e
AP_AHRS: fix example sketch
10 years ago
2deb0e08ea
AP_NavEKF: replace fabs() with fabsf()
10 years ago
79605de8f5
AP_Mission: replace fabs() with fabsf()
10 years ago
e20ffa8c75
AP_Math: replace fabs() with fabsf()
10 years ago
1c8efb25a8
AP_HAL_SITL: replace fabs() with fabsf()
10 years ago
4b6d0d8e24
AP_HAL: replace fabs() with fabsf()
10 years ago
9d74f57ed3
AP_PID: replace fabs() with fabsf()
10 years ago
70bef20a29
AC_AttitudeControl: replace fabs() with fabsf()
10 years ago
1127b716c4
SITL: lower the default noise
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prevents problems calibrating the gyro
10 years ago
2552acbf12
AP_Arming: fixed accel cal test in arming
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use a per-imu time of last cal pass, and triple accel threshold for
IMU3. Raise threshold to 0.5 for IMU1/IMU2
10 years ago
d94c95a6ef
GCS_MAVLink: return true if mission recieve is complete
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when handing a mission item, and that is the last item, return true so that whoever is handling this knows we have a new mission list. From here we can log a new mission
10 years ago
a232606fc9
AP_NavEKF: Prevent EKF yaw errors due to fast yaw spins
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Prolonged yaw rotations with gyro scale factor errors can cause yaw errors and gyro bias estimation errors to build up to a point where EKF health checks fail.
This patch introduces the following protections:
1) The assumed yaw gyro error is scaled using a filtered yaw rate and an assumed 3% scale factor error (MPU6000 data sheet)
2) When the filtered yaw rate magnitude is greater than 1 rad/sec, the Z gyro bias process noise is zeroed and the state variance set to zero to inhibit modification of the bias state
3) When the filtered yaw rate magnitude is greater than 1 rad/sec, the magnetometer quaternion corrections are scaled by a factor of four to maintain tighter alignment with the compass
10 years ago
Andrew Tridgell
Randy Mackay
Paul Riseborough
Tom Pittenger