6888545037
remove @unit enum
2016-03-25 20:33:25 -04:00
ff9b8118ab
fw_att_control add units
2016-03-25 17:24:48 -04:00
7a9427bc34
param remove empty @unit
2016-03-14 09:12:34 +01:00
344555e086
fw_att_control param @unit
2016-03-14 09:10:29 +01:00
32d062836e
Moved ECL into its own submodule
2015-12-23 06:23:15 +01:00
4df4d2ff93
code style
2015-12-11 09:49:04 +01:00
27e1aaeea5
control state: indicate if airspeed is not valid
2015-12-11 09:49:04 +01:00
18cd49292e
split FW_ATT_TC into FW_R_TC and FW_P_TC
2015-12-08 20:43:31 +01:00
f0a4979da6
Merged master into driver_framework
2015-12-01 12:34:02 +01:00
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
17653113d5
FW att control: Run all topics at full rate
2015-11-22 13:59:24 +01:00
5f40094685
fixed bug which lead to direct yaw control in stabilized mode
2015-11-17 22:28:09 +01:00
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
1ae7221593
make flaps and flaperons continuous
2015-11-17 22:28:08 +01:00
b30091be00
minor fixes
2015-11-17 22:28:08 +01:00
7fc97ed147
implemented use of flaps for auto landings
2015-11-17 22:28:08 +01:00
b16e6249e4
more correct groundspeed scaling for wheel controller
2015-11-17 22:28:08 +01:00
ff57c809b8
updated default wheel params after first test
2015-11-17 22:28:08 +01:00
e987082292
split takeoff into 2 phases, reseting integrators when still on runway
2015-11-17 22:28:08 +01:00
234a200e60
renamed heading controller to wheel controller, added groundspeed dependency and separate parameters
2015-11-17 22:28:08 +01:00
6c31421889
extracted heading controller
2015-11-17 22:28:08 +01:00
ea884b34f0
use and reset the new yaw control method
2015-11-17 22:28:07 +01:00
f43d50fbc9
implemented runway takeoff for fw
2015-11-17 22:28:07 +01:00
069c6a82cb
Merge branch 'master' of github.com:wingtra/Firmware into control_state
2015-10-16 15:50:29 +02:00
ee77ff4830
FW Att control: Avoid no symbols warnings
2015-10-14 22:36:01 +02:00
c22c678b7d
Merge branch 'master' of github.com:PX4/Firmware into control_state
2015-10-14 11:02:23 +02:00
e72e72cd65
removed vehicle_attitude subscription from fw_att_control
2015-10-14 10:53:19 +02:00
5092bcae70
fully ported control state attitude into fw_att_control
2015-10-14 09:57:41 +02:00
fb1af08234
FW att control: Remove excessive stack allocation
2015-10-10 22:23:35 +02:00
8d756055b8
integrated control state in fw_att_control
2015-10-09 08:59:05 +02:00
fa5071b3c5
Remove module.mk files to prevent confusion of adopters upgrading
2015-10-06 11:23:20 +02:00
1d6b31d196
Switch to cmake build system.
2015-09-07 20:37:45 -04:00
b4839731ad
use correct syntax for polling
2015-09-01 09:36:27 +02:00
a508330bdf
Fix attitude controller braces
2015-08-23 17:41:45 +02:00
8257f3d2fd
Replaced exits with return
2015-08-23 14:39:33 +02:00
20d71870ec
Minor changes to get fixed wing control apps running for posix
2015-08-23 14:39:25 +02:00
62269004c8
FW control: Remove unused parameters
2015-08-19 10:43:35 +02:00
04f55ce784
vtol fixes:
...
- mc pos control: publish attitude setpoint when vtol is in trans mode
- fw att control: do not publish attitude setpoint when in transition mode
- introduce flag in_transition_mode in vehicle status message for vtol
- improve tiltrotor code based on flight testing
2015-08-12 20:33:17 +02:00
809b6591c3
Bring back the ability to transition plus a partial cleanup of tiltrotor support and firefly6 config updates.
2015-08-05 16:16:03 +02:00
4cf51beb4b
FW Att control: Fix merge fail for attitude setpoint
2015-08-04 17:44:54 +02:00
420acb9748
Merge branch 'beta'
2015-08-04 10:56:53 +02:00
5b3449e75b
FW Att control: Crank up pitch default gains
2015-08-02 16:07:32 +02:00
4e1faafc9b
Remove unused variables
2015-08-02 16:07:32 +02:00
fbc1b78b38
Attitude control: Enforce rate limits by default to prevent jittery control outputs / steps
2015-08-02 16:07:32 +02:00
ea7ae7d019
Merged beta into master
2015-08-01 16:58:02 +02:00
06c45aadfb
FW attitude control: Increase default integrator gains to compensate common airframe trim issues
2015-07-19 16:03:08 +02:00
d1f8edb346
Merged beta into master
2015-07-04 23:02:47 +02:00
939d475ef2
Output flaps in all flight modes
2015-07-04 11:59:10 +02:00
ec85918e40
Set better defaults for fixed wing attitude controllers
2015-07-04 11:39:12 +02:00
454becdae5
Merged release_v1.0.0 branch into master
2015-06-25 21:45:17 +02:00
Daniel Agar