Commit Graph
420 Commits
Author SHA1 Message Date
Daniel Agar 6bb3d5f47b fw_pos_control only use const position_setpoint_triplet within control_position() 2016-03-03 10:15:40 +01:00
Daniel Agar 0cbb2c7f23 FW ALTCTL/POSCTL remove 0 throttle threshold when not landed 2016-03-03 10:14:19 +01:00
Daniel Agar d1e096abc7 more consistent naming for LND params 2016-03-03 10:13:40 +01:00
Daniel Agar 80f3fefcc3 FW adjust throttle to airspeed mapping for ALTCTL 2016-02-20 14:39:59 +01:00
Daniel Agar 4c8e9265c4 FW update position control param metadata 2016-02-20 14:37:19 +01:00
tumbili 228a54fd51 - fixed bad pitch setpoint in fw pos controller for tailsitter
- created enum for vtol types
- minor cleanup and fixes
2016-02-18 18:55:56 +01:00
Andreas Antener fe89bee02a using 0 pitch and thrust FW attitude SP when TECS isn't running 2016-02-18 18:55:56 +01:00
Andreas Antener 967b404de8 only run FW posctl in FW mode and ramp up desired airspeed for tecs after transition 2016-02-18 18:55:56 +01:00
Roman 1da686b125 TECS:
- do not run TECS for VTO which are in rotary wing mode
- reinitialise TECS the first time we start using it again
2016-02-18 18:55:56 +01:00
Lorenz Meier f10770a4a4 FW pos ctrl: Fix build error 2016-02-17 19:31:01 +01:00
Lorenz Meier e98cd6c746 FW pos control: Set idle throttle on ground in all modes 2016-02-17 19:31:01 +01:00
Andreas Antener b9b05dcc03 updated docs for FW_AIRSPD_SCALE param 2016-02-14 13:24:58 +01:00
Andreas Antener 2ff9fd64b1 increased stack sizes for mc and fw pos ctl 2016-02-11 16:53:35 +01:00
Lorenz Meier 32d9bae44d Pos control FW: Update comment 2016-02-11 14:08:58 +01:00
Roman Bapst b26fc1f089 fix waypoint handling in position control 2016-01-14 18:30:30 +01:00
Lorenz Meier bc6b640ceb FW: Fix min / max values for L1 norm 2015-12-26 16:09:24 +01:00
Lorenz Meier 32d062836e Moved ECL into its own submodule 2015-12-23 06:23:15 +01:00
Roman 4df4d2ff93 code style 2015-12-11 09:49:04 +01:00
Roman 27e1aaeea5 control state: indicate if airspeed is not valid 2015-12-11 09:49:04 +01:00
tumbili d1dc8ed432 if vtol, publish virtual attitude setpoint
Conflicts:
	src/modules/mc_pos_control/mc_pos_control_main.cpp
2015-11-25 13:28:22 +01:00
Roman 120fd9d522 use control state topic for attitude and airspeed 2015-11-17 22:28:09 +01:00
Andreas Antener d97ead81aa set talt timeout to 10sec 2015-11-17 22:28:09 +01:00
Andreas Antener 5b1c7321e7 reverted navigation on landing back to old heading hold 2015-11-17 22:28:09 +01:00
Roman 6f4c8d45ff during flare control pitch setpoint based on distance to ground 2015-11-17 22:28:09 +01:00
Roman 7f0c3a9b71 use virtual setpoint for landing line tracking 2015-11-17 22:28:09 +01:00
Roman 3d3398e330 added code handling aborting landings 2015-11-17 22:28:09 +01:00
tumbili 0bd23dd7c5 only go into heading hold mode after flaring 2015-11-17 22:28:09 +01:00
tumbili 73b1c18698 do not stick to terrain estimate if it's not valid 2015-11-17 22:28:09 +01:00
Andreas Antener 4e22d65325 don't use virtual line anymore for takeoff but use correct starting point to navigate, updated default parameters for wheel controller 2015-11-17 22:28:09 +01:00
Andreas Antener 5949b6615d don't reset the yaw integrator on takeoff 2015-11-17 22:28:09 +01:00
tumbili f3e0d91f24 added airspeed scale parameter for takeoff and landing 2015-11-17 22:28:08 +01:00
tumbili 42d03cb076 activate wheel controller as soon as plane flares 2015-11-17 22:28:08 +01:00
tumbili 7fc97ed147 implemented use of flaps for auto landings 2015-11-17 22:28:08 +01:00
Andreas Antener e0cdf65fb4 use navigator to hold heading 2015-11-17 22:28:08 +01:00
Andreas Antener d015fbd678 added startup config for Maja and new generic mixer that uses channel 5 for wheel steering 2015-11-17 22:28:08 +01:00
Andreas Antener 0769ec5345 added max pitch parameter for climbout phase 2015-11-17 22:28:08 +01:00
Andreas Antener e987082292 split takeoff into 2 phases, reseting integrators when still on runway 2015-11-17 22:28:08 +01:00
Andreas Antener 234a200e60 renamed heading controller to wheel controller, added groundspeed dependency and separate parameters 2015-11-17 22:28:08 +01:00
Andreas Antener 6c31421889 extracted heading controller 2015-11-17 22:28:08 +01:00
Andreas Antener 51ef854173 extracted runway takeoff logic into external class 2015-11-17 22:28:08 +01:00
Andreas Antener 1f8ebb71f5 fix comment 2015-11-17 22:28:08 +01:00
Andreas Antener b93f34c99b use separate heading parameter beacause the other one gets reset in auto 2015-11-17 22:28:08 +01:00
Andreas Antener 24179a0d93 consitent parameter naming for runway takeoff, added parameters for important values 2015-11-17 22:28:08 +01:00
Andreas Antener ea884b34f0 use and reset the new yaw control method 2015-11-17 22:28:07 +01:00
Andreas Antener 059e40f780 - fixed throttle ramp-up
- added parameter to specify which heading to keep on runway
- validate terrain alt before using it
2015-11-17 22:28:07 +01:00
tumbili f43d50fbc9 implemented runway takeoff for fw 2015-11-17 22:28:07 +01:00
Youssef Demitri 170f0032fd updated to master (solve merge conflicts) 2015-11-06 12:18:31 +01:00
Lorenz Meier eeecf01628 Fixed wing controller: Call state reset on flight mode change. 2015-11-01 18:26:30 +01:00
Youssef Demitri dd59409e31 updated to master (solved merge conflicts) 2015-10-27 09:26:27 +01:00
jgoppert 6cce823dc6 Replaced wigen with custom matrix lib. 2015-10-24 15:10:20 -04:00