ardupilot

Commit Graph

Author	SHA1	Message	Date
Randy Mackay	6f6c9e2585	AC_PosControl: bug fix to vertical speed limit Vehicle was not reaching target climb or descent rate because of incorrectly defaulted acceleration	11 years ago
Andrew Tridgell	25667a11a0	AP_NavEKF: use AHRS vehicle class for sideslip calculation Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
Andrew Tridgell	5acd17b843	AP_NavEKF: cleanup some build warnings Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
Andrew Tridgell	c8c6e05a4a	AP_AHRS: added vehicle class to AHRS used by EKF to control use of get_fly_forward()	11 years ago
priseborough	bd28cdbdcf	AP_NavEKF: Improved magnetometer consistency checks A magnetometer axis that fails the innovation consistency check will cause all axes not to be used. If this condition continues for 10 seconds, a magnetometer timeout condition will be declared. When the timeout has occurred, if it is not a fly forward vehicle, then individual channels will be used again, but with a reduced weighting.	11 years ago
Randy Mackay	648787a6c8	AC_WPNav: rename some definitions	11 years ago
Randy Mackay	2167dd7d3e	AC_WPNav: update target speed immediately	11 years ago
Andrew Tridgell	05bffb5915	HAL_SITL: enable use of SIM_FLOAT_EXCEPT parameter	11 years ago
Andrew Tridgell	e0db7b117f	SITL: added SIM_FLOAT_EXCEPT parameter this enables checking for floating point exceptions	11 years ago
Andrew Tridgell	610a930612	AP_NavEKF: catch covarience errors and reset filter this catches covariance values beyond a reasonable limit and resets the filter is they happen	11 years ago
Andrew Tridgell	7e5a491f14	AP_Math: prevent a floating point exception	11 years ago
Andrew Tridgell	4d24a86088	AP_AHRS: prevent a infinity value	11 years ago
Randy Mackay	d382fa51ee	AC_WPNav: run loiter and wp nav at 50hz on Pixhawk	11 years ago
Randy Mackay	72d2712c4e	AC_WPNav: integrate update_xy_controller name change	11 years ago
Randy Mackay	966340a02a	Circle: integrate update_xy_controller name change	11 years ago
Randy Mackay	7e376bc517	PosControl: update_pos_controller renamed to update_xy_controller	11 years ago
Andrew Tridgell	4756dbee84	AP_NavEKF: fixed millisecond subtraction for rollover Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
Andrew Tridgell	be9d0c1c4d	APM_OBC: setup termination values in PX4IO this sets up the PX4IO board with failsafe values in case the FMU is not running	11 years ago
Andrew Tridgell	0d4985079e	RC_Channel: added support for LimitValue settings this allows you to set a channel failsafe or radio_out to a limit value	11 years ago
Andrew Tridgell	7f4178d967	RC_Channel: added setup_failsafe_trim_all() function sets all channels to output trim values on FMU failure	11 years ago
Andrew Tridgell	5cd145a307	AP_HAL: added set_failsafe_pwm() API this allows the PWM values for FMU firmware failure to be setup	11 years ago
Andrew Tridgell	7f9a9107c7	APM_Control: logging_started needs to be static prevents writing log headers twice	11 years ago
Andrew Tridgell	68f1ae3036	AP_NavEKF: fixed some matlab ! -> ~ typos Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
Andrew Tridgell	5a7afbf2cd	AP_GPS: prevent writing GPS log headings multiple times	11 years ago
Randy Mackay	e3ffd5c0dd	Common: remove RallyLocation defintion	11 years ago
Randy Mackay	7011ab40c2	Rally: define RALLY_WP_SIZE and RallyLocation	11 years ago
Michael Day	a2aab2ab5e	AP_Rally: Minor fixes to AP_Rally after initial testing - If a Rally point is being used, always respect the altitude set by the user (don't take the max of that and the home point altitude). - No need for constructor to pass in size of RallyLocation struct	11 years ago
Andrew Chapman	5825bac410	AP_Rally library	11 years ago
Randy Mackay	5322093475	Mission: fix example sketch after GPS lib changes	11 years ago
Andrew Tridgell	b4c5f31b17	APM_Control: reduce the number of parameter saves in autotune don't save a parameter unless it has changed by 0.1%	11 years ago
Paul Riseborough	ccc7d36493	APM_Control: Modify D and I gain scaling	11 years ago
Randy Mackay	94d38ee294	AC_Circle: add get_closest_point_on_circle init_start_angle method added to use current heading or position to decide on initial start angle	11 years ago
Kevin Hester	c2184cb8e4	PID: fixup line endings	11 years ago
Kevin Hester	72e97cbf5c	AP_Param: fixup line endings	11 years ago
Kevin Hester	a7820e6c71	OptFlow: fixup line endings	11 years ago
Kevin Hester	fce1277b0e	Notify: fixup line endings	11 years ago
Kevin Hester	b7bed437c2	Compass: fixup line endings	11 years ago
Kevin Hester	80cb13e222	BattMon: fixup line endings	11 years ago
Kevin Hester	d09e871319	AP_Airspeed: fixup line endings	11 years ago
Kevin Hester	c34c4d79f6	AP_ADC: fixup line endings	11 years ago
Kevin Hester	b7410494e3	AC_PID: fixup line endings	11 years ago
L. Preston Sego III	3ecdc4b741	Copter: Add support for V-Tail Quads	11 years ago
Randy Mackay	02775e8dc5	AC_PosControl: get_accel_target returns const ref	11 years ago
Randy Mackay	60f522a094	AC_WPNav: set_wp_destination to use current target Previously we used the projected stopping point if the vehicle had not reached the destination but this could lead to large jumps in target position	11 years ago
Andrew Tridgell	ae7293ef68	APM_Control: added support for AUTOTUNE_LEVEL 10 levels of tune, for what type of tune the user wants	11 years ago
Andrew Tridgell	86f167fc7f	AP_Vehicle: added autotune_level to fixed wing parms	11 years ago
Andrew Tridgell	b7350118a6	AP_AHRS: enable EKF wind estimate with no airspeed sensor EKF can now estimate with IMU and GPS only Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
Andrew Tridgell	4abc2999a6	AP_NavEKF: start with a wind estimate of 3m/s, when no direct measurement this will cope better with users with low roll/pitch gains, to ensure they get enough control on takeoff Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>	11 years ago
priseborough	d745dc2b6f	AP_NavEKF : Increased position gate default to reduce impact of accel errors Flight testing with windup turns has shown that the position gate threshold can be tripped with good GPS data causing position jerks. This increases the initial GPS glitch rejection threshold to effectively 5m when using the default POSNE_NOISE value of 0.5m.	11 years ago
priseborough	188bea6bab	AP_NavEKF : Enable calc of wind velocity when not using airspeed sensing This patch also cleans up the logic associated with use of the synthetic sideslip measurement so that it can never be used for a non fly-forward vehicle type This patch adds functionality that initialises the wind-speed vector to the reciprocal of the ground speed vector, and scaled to 6 m/s. On average this gives a better initial wind velocity estimate on launch by assuming: a) launch will be into wind b) wind speed is equal to global average It also helps prevent a headwind causing initial underestimation of airspeed causing high autopilot gains and limit cycles on climb-out, until first turn when the EKF is able to estimate the wind.	11 years ago

1 2 3 4 5 ...

5158 Commits (5fc071f5f9bf25ccc14efa60498f6bbb9bc49889)