px4_autopilot

Commit Graph

Author	SHA1	Message	Date
Paul Riseborough	b0300b9723	Revert "attitude_fw delete unused and cleanup" This reverts commit `25bd3ac5e6`.	8 years ago
Daniel Agar	25bd3ac5e6	attitude_fw delete unused and cleanup	8 years ago
Daniel Agar	e7ed32fb82	attitude_fw remove extra semicolons	8 years ago
Andreas Antener	66b8f7ec5b	Removed obsolete fields from ECL control data	8 years ago
Andreas Antener	5363e8d307	Wheel controller: use library function to wrap pi	8 years ago
Daniel Agar	674ab3f81b	attitude_fw fix style	8 years ago
Roman	f22ad30ef3	removed turn compensation flag form control data since it's obsolete Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	e1f9874c82	wheel controller: fix computation and scaling of integrator Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	c4cc02b3f2	yaw controller: fix bug where roll for turn coordination was constrained wrongly Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	391b6dfd00	yaw controller: for now do not do turn compensation when inverted and use the roll setpoint as limit for turn compensation Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	66b7773059	yaw controller: deactivate lateral acceleration control for now but put comment of how to do it properly Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	f300877db4	yaw controller: computed desired yaw rate based on coordinated turn constraint Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	4057defa53	pitch controller: removed turn offset compensation form pitch controller - turn compensation is included in the desired yawrate Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	55401ec1b0	fw attitude control: compute integrator correctly - I gain was applied wrongly, such that the integrator value was depending direcly on the I gain. This made the integrator value jump when the gain was changed Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Roman	ac7fc30ea7	fw attitude controllers: restructuring in order to allow acro flight mode - split rate control into body rate control and euler rate control - this allows standard attitude control but also direct rate control of all three axes - allow activation/deactivation of turn compensation Signed-off-by: Roman <bapstroman@gmail.com>	8 years ago
Daniel Agar	2750961be6	c++11 initialization cleanup (#237 )	8 years ago
Daniel Agar	47b8ef258b	clang-tidy performance-type-promotion-in-math-fn (#236 )	8 years ago
Lorenz Meier	10c6ae77ae	Attitude fw yaw: Initialize yaw rate properly	8 years ago
Daniel Agar	983c44088f	fw att fix pitch feedforward constrained roll	8 years ago
Daniel Agar	0d02bb2612	ecl attitude_fw fix excessive body fixed turn offset -limit body fixed turn offset contrained roll to possible roll setpoint range -fixes #181	8 years ago
Lorenz Meier	199c423f1f	Attitude fw: Remove builtin perf counters	9 years ago
Daniel Agar	82cf1827d4	fw multiply integrator gain in loop	9 years ago
Lorenz Meier	699ec17cc3	Removed spurious print in wheel controller	9 years ago
Roman	3c7705b3f9	checked out attitude fw folder from master	9 years ago
Lorenz Meier	e5743d503c	Initial import	9 years ago

25 Commits (bba3f70a0e3a0a63271e6f76ec169148723991c9)