28 Commits

Author	SHA1	Message	Date
Andrew Tridgell	2297c6bcd2	AP_TECS: added TECS_LAND_SINK parameter ... this controls the sink rate for the final stage of landing	2014-08-13 21:38:05 +10:00
Andrew Tridgell	7c4d31c481	AP_TECS: added TECS_PITCH_MAX and TECS_PITCH_MIN ... this allows the TECS controlled pitch limits to be smaller than the FBWA limits. It is common for a human pilot to want a bit more discretion over pitch than you want the automatic controller to use	2014-08-06 17:59:18 +10:00
Andrew Tridgell	e24febec1b	AP_TECS: avoid a valgrind bug	2014-07-14 09:44:35 +10:00
Michael Day	312a2fc8dc	AP_TECS: Parameter TECS_LAND_SPDWGT allows custom landing speed weight.	2014-04-10 15:42:49 +10:00
Andrew Tridgell	a55c4e2296	AP_TECS: set target airspeed, not min/max airspeed, on landing ... this seems to prevent ballooning of the altitude when we are in the landing approach, and gives a much smoother landing	2014-03-20 17:34:39 +11:00
Michael Day	bd7e1b82e1	AP_TECS: Auto landing now takes throttle_nudge into account.	2014-03-20 17:34:26 +11:00
Michael Day	861690dea2	AP_TECS: New params LAND_ARSPD and LAND_THR auto-slowing landings. ... Also controlling pitch by ignoring height error during landing. This serves to keep the nose up.	2014-03-20 17:34:23 +11:00
Paul Riseborough	88b0364fcd	AP_TECS : Add protection for airspeed runaway due to pitch errors	2014-03-09 19:59:16 +11:00
Andrew Tridgell	9b8311580b	AP_TECS: update for AHRS API change	2014-02-15 05:48:24 +11:00
Paul Riseborough	9bbddb2f66	AP_TECS : Use NavEKF height and height rate data if available	2014-02-15 05:48:21 +11:00
Paul Riseborough	bc311542ab	AP_TECS : Fixed bug preventing accel launch detection when not using AS sensor	2014-02-07 19:20:54 +11:00
Paul Riseborough	585d61b960	AP_TECS : Reduce tendency to overspeed during climbout ... The old code relies on the action of the integrator to raise the nose above the minimum pitch angle which depending on the model and the tuning can be too slow to correct. Biasing the pitch angle to climbout minimum will reduce the taken before an overspeed condition is corrected.	2013-12-20 09:43:04 +11:00
Andrew Tridgell	b096881f81	AP_TECS: added time to TECS messages	2013-11-04 21:36:40 +11:00
Andrew Tridgell	28a4b6ad9f	AP_TECS: update for AHRS API change	2013-11-04 21:21:42 +11:00
Andrew Tridgell	84336bc74e	AP_TECS: added initial flight_stage handling	2013-10-12 13:12:43 +11:00
Andrew Tridgell	3c967a9c71	AP_TECS: use a ahrs reference ... saves a pointer access	2013-08-14 14:58:49 +10:00
Paul Riseborough	34f0af25cc	AP_TECS : Improvements and bug fixes to feed-forward throttle demand ... This fixes a bug in the feed-forward throttle that prevented the bank to throttle compensation from working properly during descents. It also adds bank to throttle compensation to the non-airspeed sensor throttle algorithm.	2013-08-02 21:47:01 +10:00
Andrew Tridgell	620d067ee1	AP_TECS: use ahrs EAS2TAS for true airspeed	2013-07-22 12:50:01 +10:00
Andrew Tridgell	fb0e48a25d	AP_TECS: adapt for new airspeed variable names	2013-07-18 14:53:23 +10:00
Paul Riseborough	66d60953df	TECS: added height update_pitch call	2013-07-10 14:04:22 +10:00
Paul Riseborough	2c5db9a165	TECS: added support for throttle nudging	2013-07-09 20:50:37 +10:00
Paul Riseborough	9c431b4a04	TECS: use altitude supplied by mainline code ... this allows for use of ALT_OFFSET and ALT_MIX	2013-07-09 09:25:53 +10:00
Paul Riseborough	a694b781c7	AP_TECS: Add non airspeed sensor pitch to throttle mode lost during integration	2013-07-05 22:16:39 +10:00
Andrew Tridgell	87f6cc715d	AP_TECS: fixed parameter doc formatting	2013-07-04 17:52:40 +10:00
Paul Riseborough	8082122053	TECS-WIP : Fixed bug in initialisation of DT value	2013-07-04 16:57:50 +10:00
Andrew Tridgell	904e6b5b8f	AP_TECS: for _DT to at most 0.1	2013-07-04 16:56:57 +10:00
Andrew Tridgell	68232a10f9	AP_TECS: updates to use new aircraft parameter structure	2013-07-04 16:56:57 +10:00
Paul Riseborough	5b0129e02b	AP_TECS: first implemention of TECS altitude control library	2013-07-04 16:56:56 +10:00