Daniel Agar
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7c5ba19fe2
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fw_pos_control_l1 param @unit
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2016-03-14 09:10:29 +01:00 |
|
Daniel Agar
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fa66055a92
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mTecs param @unit
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2016-03-14 09:10:29 +01:00 |
|
Lorenz Meier
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7871ab0fae
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Fixed wing: support do change speed
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2016-03-13 18:08:25 +01:00 |
|
Daniel Agar
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6bb3d5f47b
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fw_pos_control only use const position_setpoint_triplet within control_position()
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2016-03-03 10:15:40 +01:00 |
|
Daniel Agar
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0cbb2c7f23
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FW ALTCTL/POSCTL remove 0 throttle threshold when not landed
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2016-03-03 10:14:19 +01:00 |
|
Daniel Agar
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d1e096abc7
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more consistent naming for LND params
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2016-03-03 10:13:40 +01:00 |
|
Daniel Agar
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80f3fefcc3
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FW adjust throttle to airspeed mapping for ALTCTL
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2016-02-20 14:39:59 +01:00 |
|
Daniel Agar
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4c8e9265c4
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FW update position control param metadata
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2016-02-20 14:37:19 +01:00 |
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tumbili
|
228a54fd51
|
- fixed bad pitch setpoint in fw pos controller for tailsitter
- created enum for vtol types
- minor cleanup and fixes
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2016-02-18 18:55:56 +01:00 |
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Andreas Antener
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fe89bee02a
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using 0 pitch and thrust FW attitude SP when TECS isn't running
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2016-02-18 18:55:56 +01:00 |
|
Andreas Antener
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967b404de8
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only run FW posctl in FW mode and ramp up desired airspeed for tecs after transition
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2016-02-18 18:55:56 +01:00 |
|
Roman
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1da686b125
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TECS:
- do not run TECS for VTO which are in rotary wing mode
- reinitialise TECS the first time we start using it again
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2016-02-18 18:55:56 +01:00 |
|
Lorenz Meier
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f10770a4a4
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FW pos ctrl: Fix build error
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2016-02-17 19:31:01 +01:00 |
|
Lorenz Meier
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e98cd6c746
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FW pos control: Set idle throttle on ground in all modes
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2016-02-17 19:31:01 +01:00 |
|
Andreas Antener
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b9b05dcc03
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updated docs for FW_AIRSPD_SCALE param
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2016-02-14 13:24:58 +01:00 |
|
Andreas Antener
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2ff9fd64b1
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increased stack sizes for mc and fw pos ctl
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2016-02-11 16:53:35 +01:00 |
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Lorenz Meier
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32d9bae44d
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Pos control FW: Update comment
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2016-02-11 14:08:58 +01:00 |
|
Roman Bapst
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b26fc1f089
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fix waypoint handling in position control
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2016-01-14 18:30:30 +01:00 |
|
Lorenz Meier
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bc6b640ceb
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FW: Fix min / max values for L1 norm
|
2015-12-26 16:09:24 +01:00 |
|
Lorenz Meier
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32d062836e
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Moved ECL into its own submodule
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2015-12-23 06:23:15 +01:00 |
|
Roman
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4df4d2ff93
|
code style
|
2015-12-11 09:49:04 +01:00 |
|
Roman
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27e1aaeea5
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control state: indicate if airspeed is not valid
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2015-12-11 09:49:04 +01:00 |
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tumbili
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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
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use control state topic for attitude and airspeed
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2015-11-17 22:28:09 +01:00 |
|
Andreas Antener
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d97ead81aa
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set talt timeout to 10sec
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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
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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
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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
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2015-11-17 22:28:08 +01:00 |
|
tumbili
|
42d03cb076
|
activate wheel controller as soon as plane flares
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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 |
|