ardupilot

Commit Graph

Author	SHA1	Message	Date
Randy Mackay	7056484ef0	Copter: fix spline overshoot	10 years ago
Randy Mackay	56b92e7d8c	AC_PID: fix example sketch	10 years ago
Paul Riseborough	c2ac80cc63	AP_AHRS: Prevent copter from switching to DCM unless EKF has severe errors	10 years ago
Randy Mackay	3f8b832075	InertialSensor: fix example sketch	10 years ago
Randy Mackay	3bcd97fcd1	Parachute: increase deployment duration to 2sec	10 years ago
Randy Mackay	5560d3dba1	BattMonitor: fix example sketch	10 years ago
Randy Mackay	e080b2acce	AP_Arming: use accel_calibrated_ok_all	10 years ago
Randy Mackay	1f14eec4ea	InertialSensor: accel_calibrated_all_ok replaces calibrated 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
Randy Mackay	0d72f3ac29	AP_HAL: fix example sketches	10 years ago
Andrew Tridgell	8bf2baef70	AP_InertialSensor: fixed primary accel/gyro in replay	10 years ago
Andrew Tridgell	f40c96de9d	SITL: add 'quad' and 'copter' as aliases for quadcopter	10 years ago
Andrew Tridgell	2a47cc3c81	HAL_SITL: cleanup command line handling	10 years ago
Andrew Tridgell	bab94c8a04	SITL: close high fds before launching JSBSIM	10 years ago
Andrew Tridgell	414f4125de	AP_HAL: use FD_CLOEXEC to prevent sockets being inherited in SITL	10 years ago
Andrew Tridgell	7692889248	SIM_JSBSim: added elevon and vtail support	10 years ago
Andrew Tridgell	aa9853179c	SITL: fixed startup yaw	10 years ago
Andrew Tridgell	5687adbdba	HAL_SITL: support JSBSim backend	10 years ago
Andrew Tridgell	692fc18698	AP_HAL: protect Socket.h from double include	10 years ago
Andrew Tridgell	c136d65c25	SITL: added initial JSBSim simulator backend	10 years ago
Andrew Tridgell	8ec98a5ec9	SITL: make it possible to connect two SITL instances together this adds --client to set uartC as a tcp client rather than a TCP server	10 years ago
Andrew Tridgell	3991e0c476	DataFlash: fixed sign of sv in GRAW message	10 years ago
Andrew Tridgell	3529e02675	AP_AHRS: if we have 3 gyros then only use first two the 3rd gyro on a PH2 has a lot more noise as it is not vibration isolated	10 years ago
Paul Riseborough	cb59570938	AP_NavEKF: Remove bug preventing external selection of optical flow mode	10 years ago
Randy Mackay	3390d9932e	AP_AHRS: fix example sketch	10 years ago
Tom Pittenger	2deb0e08ea	AP_NavEKF: replace fabs() with fabsf()	10 years ago
Tom Pittenger	79605de8f5	AP_Mission: replace fabs() with fabsf()	10 years ago
Tom Pittenger	e20ffa8c75	AP_Math: replace fabs() with fabsf()	10 years ago
Tom Pittenger	1c8efb25a8	AP_HAL_SITL: replace fabs() with fabsf()	10 years ago
Tom Pittenger	4b6d0d8e24	AP_HAL: replace fabs() with fabsf()	10 years ago
Tom Pittenger	9d74f57ed3	AP_PID: replace fabs() with fabsf()	10 years ago
Tom Pittenger	70bef20a29	AC_AttitudeControl: replace fabs() with fabsf()	10 years ago
Andrew Tridgell	1127b716c4	SITL: lower the default noise prevents problems calibrating the gyro	10 years ago
Andrew Tridgell	2552acbf12	AP_Arming: fixed accel cal test in arming 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
Tom Pittenger	d94c95a6ef	GCS_MAVLink: return true if mission recieve is complete 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
Paul Riseborough	a232606fc9	AP_NavEKF: Prevent EKF yaw errors due to fast yaw spins 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
Paul Riseborough	08382373f1	AP_NavEKF: Reduce likelihood of in-air switch to GPS with a bad heading Increases magnetometer weighting on yaw corrections when there there is no other aiding to constrain yaw drift. Prevents switch to GPS if magnetometer data is failing innovation checks which indicates a bad yaw angle	10 years ago
Randy Mackay	3781f133d7	AC_AttControlHeli: remove unused definitions	10 years ago
Randy Mackay	bef5633ed5	AC_AttControlHeli: use params from parent class	10 years ago
Randy Mackay	7951346d72	AC_AttControl: bf_feedfoward_save made more concise	10 years ago
Randy Mackay	3d9a6a69e2	MotorsHeli: COLYAW to float	10 years ago
Randy Mackay	edfa206bb8	Motors_Heli: nest heli params	10 years ago
Randy Mackay	68b05a4ca2	AP_Motors: is_throttle_mix_min returns bol	10 years ago
Leonard Hall	cf45a1cf3a	AC_AttitudeControl: add get accel and save ff	10 years ago
Leonard Hall	1900cc7582	AC_AttitudeControl: Enable FF by default	10 years ago
Leonard Hall	0f894ac1a8	AP_Motors: Rename and move Throttle Mix / Comp	10 years ago
Jonathan Challinger	142e018a18	AP_NavEKF: fix bug causing takeoff to fail	10 years ago
Randy Mackay	fa4ba456b4	GPS: fix example sketches	10 years ago
Andrew Tridgell	afc9812d0b	AP_InertialSensor: update VibTest after moving messages info DataFlash	10 years ago
Andrew Tridgell	7d90033a36	AP_InertialSensor: support raw accel and gyro dataflash logging	10 years ago
Andrew Tridgell	21d805422d	DataFlash: added defines for raw accel and gyro logging	10 years ago

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7935 Commits (e589ca9b80cc8aadfd4910e0469b62c01ffaeff5)