tumbili
5f40094685
fixed bug which lead to direct yaw control in stabilized mode
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
tumbili
1ae7221593
make flaps and flaperons continuous
2015-11-17 22:28:08 +01:00
tumbili
b30091be00
minor fixes
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
b16e6249e4
more correct groundspeed scaling for wheel controller
2015-11-17 22:28:08 +01:00
Andreas Antener
ff57c809b8
updated default wheel params after first test
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
ea884b34f0
use and reset the new yaw control method
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
069c6a82cb
Merge branch 'master' of github.com:wingtra/Firmware into control_state
2015-10-16 15:50:29 +02:00
Lorenz Meier
ee77ff4830
FW Att control: Avoid no symbols warnings
2015-10-14 22:36:01 +02:00
Youssef Demitri
c22c678b7d
Merge branch 'master' of github.com:PX4/Firmware into control_state
2015-10-14 11:02:23 +02:00
Youssef Demitri
e72e72cd65
removed vehicle_attitude subscription from fw_att_control
2015-10-14 10:53:19 +02:00
Youssef Demitri
5092bcae70
fully ported control state attitude into fw_att_control
2015-10-14 09:57:41 +02:00
Lorenz Meier
fb1af08234
FW att control: Remove excessive stack allocation
2015-10-10 22:23:35 +02:00
Youssef Demitri
8d756055b8
integrated control state in fw_att_control
2015-10-09 08:59:05 +02:00
Lorenz Meier
fa5071b3c5
Remove module.mk files to prevent confusion of adopters upgrading
2015-10-06 11:23:20 +02:00
James Goppert
1d6b31d196
Switch to cmake build system.
2015-09-07 20:37:45 -04:00
tumbili
b4839731ad
use correct syntax for polling
2015-09-01 09:36:27 +02:00
Lorenz Meier
a508330bdf
Fix attitude controller braces
2015-08-23 17:41:45 +02:00
devbharat
8257f3d2fd
Replaced exits with return
2015-08-23 14:39:33 +02:00
devbharat
20d71870ec
Minor changes to get fixed wing control apps running for posix
2015-08-23 14:39:25 +02:00
Lorenz Meier
62269004c8
FW control: Remove unused parameters
2015-08-19 10:43:35 +02:00
tumbili
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
Simon Wilks
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
Lorenz Meier
4cf51beb4b
FW Att control: Fix merge fail for attitude setpoint
2015-08-04 17:44:54 +02:00
Lorenz Meier
420acb9748
Merge branch 'beta'
2015-08-04 10:56:53 +02:00
Lorenz Meier
5b3449e75b
FW Att control: Crank up pitch default gains
2015-08-02 16:07:32 +02:00
Lorenz Meier
4e1faafc9b
Remove unused variables
2015-08-02 16:07:32 +02:00
Lorenz Meier
fbc1b78b38
Attitude control: Enforce rate limits by default to prevent jittery control outputs / steps
2015-08-02 16:07:32 +02:00
Lorenz Meier
ea7ae7d019
Merged beta into master
2015-08-01 16:58:02 +02:00
Lorenz Meier
06c45aadfb
FW attitude control: Increase default integrator gains to compensate common airframe trim issues
2015-07-19 16:03:08 +02:00
Lorenz Meier
d1f8edb346
Merged beta into master
2015-07-04 23:02:47 +02:00
Lorenz Meier
939d475ef2
Output flaps in all flight modes
2015-07-04 11:59:10 +02:00
Lorenz Meier
ec85918e40
Set better defaults for fixed wing attitude controllers
2015-07-04 11:39:12 +02:00
Lorenz Meier
454becdae5
Merged release_v1.0.0 branch into master
2015-06-25 21:45:17 +02:00
tumbili
4e9fd5b2a4
rotate attitude for fw mode only if VTOL is a tailsitter
2015-06-19 09:25:16 +02:00
Lorenz Meier
c9fefe236b
Merged release into master
2015-06-13 11:06:01 +02:00
Lorenz Meier
8838b18da7
FW attitude control: Run attitude controller as fast as we can to minimize latency
2015-06-12 16:10:20 +02:00
Lorenz Meier
90362a9889
FW attitude controller: Fix usage of trim parameters to apply only to the final outputs
2015-06-09 14:16:37 +02:00
Lorenz Meier
46d969772c
Fixed wing heading hold: Engage only after wings got close to level already
2015-06-05 22:45:07 +02:00
Lorenz Meier
21fde4b3f6
fw att control: Code style fixes
2015-06-05 22:45:06 +02:00
Lorenz Meier
5197be67a7
FW control: Add skeleton for distinct altitude control and position control flight modes
...
Conflicts:
src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp
2015-06-05 22:45:05 +02:00
tumbili
134c7d87b8
do not run fw attitude controller when in rotary wing mode (VTOL)
2015-05-30 15:39:37 +02:00
Mark Charlebois
1ca05aaa64
orb_advert_t changed to void * and checks changed to nullptr
...
The existing orb_advert_t use thoughout the code sometimes tries
to treat it as a file descriptor and there are checks for < 0
and ::close calls on orb_advert_t types which is an invalid use
of an object pointer, which is what orb_advert_t really is.
Initially I had changed the -1 initializations to 0 but it was
suggested that this should be nullptr. That was a good recommendation
but the definition of orb_advert_t had to change to void * because
you cannot initialize a uintptr_t as nullptr.
Signed-off-by: Mark Charlebois <charlebm@gmail.com >
2015-05-27 14:42:49 -07:00
Mark Charlebois
a734fc96d1
extensive orb_advert_t fixes
...
The calls to orb_advertise were being mishandled throughout the code.
There were ::close() calls on memory pointers, there were checks
against < 0 when it is a pointer to a object and values larger than
0x7ffffffff are valid. Some places orb_advert_t variables were
being initialized as 0 other places as -1.
The orb_advert_t type was changed to uintptr_t so the pointer value
would not be wrapped as a negative number. This was causing a failure
on ARM.
Tests for < 0 were changed to == 0 since a null pointer is the valid
representation for error, or uninitialized.
Signed-off-by: Mark Charlebois <charlebm@gmail.com >
2015-05-27 14:41:33 -07:00
Ban Siesta
96bfe85ceb
fw_att_control: another ugly way to prevent a newline
2015-05-26 23:05:26 -07:00
tumbili