0dfd8cd039
Update fw_att_control_main.cpp
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Make the declarations of the variables "roll_sp, pitch_sp, yaw_sp, throttle_sp," in the main loop more readable.
2017-06-04 18:17:29 +08:00
64ed96d81a
clang-tidy readability-simplify-boolean-expr
2017-06-02 19:35:18 -04:00
c5e0bf1c2f
uORB combine VTOL FW and MC virtual topics ( #7008 )
2017-04-09 13:17:20 -04:00
e63ee9d8bd
fw_att wheel controller enable param (default off)
2017-03-05 11:41:14 +08:00
1b2973f602
VTOL fw_att don't reset integrators during transition
2017-02-25 17:57:05 +01:00
ecb2511a7b
add matrix copyTo
2017-02-25 11:04:02 +01:00
e81e6a8296
fw_att_control add rattitude mode
2017-02-18 08:03:19 +01:00
9120082b0c
fw_att_control stabilized mode publish att_sp quat
2017-02-18 08:03:19 +01:00
12e5aca028
fw_att_control remove unused accel sub
2017-02-18 08:03:19 +01:00
459b8b7c7e
FW att: removed unused fields again
2017-02-18 08:03:19 +01:00
b19cd19411
FW Acro: udpate ECL and implemented fixed-wing Acro
2017-02-18 08:03:19 +01:00
51c8e90508
FW att control: Increase stack size to ensure limits
2017-02-17 22:31:55 +01:00
7a77e27a79
fixed wing offboard attitude setpoint fix ( #6112 )
2017-02-15 23:51:50 -05:00
e927f3e040
clang-tidy modernize-use-nullptr
2017-02-01 22:15:50 -05:00
b721f5fc7c
fw_att_control init all fields and delete unused
2017-01-04 16:08:20 -05:00
8defe7e7d9
Revert scaling change
2016-12-26 16:56:22 +01:00
ba3796ebaf
Work with double scaling
2016-12-26 16:56:22 +01:00
17a089af31
Fix orb poll
2016-12-26 16:56:22 +01:00
7fd5aae834
Apply battery voltage throttle scaling to FW (ported from #5778 )
2016-12-26 16:56:22 +01:00
93fb02bfa3
fw_att_ctrl: Code cleanup
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Signed-off-by: CarlOlsson <carlolsson.co@gmail.com >
2016-10-31 15:17:14 +01:00
2fff2ab9ac
Add switch for landing gear, pass it to actuators
2016-10-20 23:17:05 +02:00
241fd629ce
ERROR macro: get rid of the many 'oddly, ERROR is not defined for c++', use PX4_ERROR
2016-09-30 13:50:51 +02:00
8ff237c69f
Remove size optimization for individual modules
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It makes more sense to set the optimization flags on a platform basis
instead of individually for each module. This allows for different
optimization options for SITL, NuttX, Snapdragon, etc.
2016-09-30 08:11:51 +02:00
670697b0ac
fw_att_control_main: fix implicit float to double conversion issue
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GCC 6.1.1 output:
../src/modules/fw_att_control/fw_att_control_main.cpp:884:41: error:
implicit conversion from ‘float’ to ‘double’ to match other operand of
binary expression [-Werror=double-promotion]
2016-09-13 11:43:22 +02:00
3163cf90c9
FW: simplified flap/flaperon logic and always move them at the same rate (don't jump)
2016-09-07 19:29:32 +02:00
2dd29ec4a1
VTOL: publish stabilized FW attitude to correct topic
2016-08-06 20:43:49 +02:00
aea7bd5b47
fw_attitude_control: calculate attitude setpoint for STAB mode
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- attitude setpoint generation for stabilized mode was shifted back
to the fw attitude controller. since the fw position controller is polling
on global position attitude setpoints were not generated when global
position was not published.
Signed-off-by: Roman <bapstroman@gmail.com >
2016-07-25 08:56:19 +02:00
0a997577f5
allow manual yaw in all manual modes and also use it as threshold to snap into heading lock
2016-07-25 08:56:19 +02:00
fd51bf44d5
fw position / fw attitude control: move attitude setpoint generation to
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position controller
- attitude setpoints for all modes are now computed in the fw position
controller
Signed-off-by: tumbili <roman@px4.io >
2016-07-25 08:56:18 +02:00
f0dd5a103c
allow scaling controls in full manual mode for fixed wings
2016-07-13 09:29:12 +02:00
784883af22
added parameters to allow scaling controls in full manual mode
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for fixed wings
2016-07-13 09:29:12 +02:00
099becb353
added parameter for airspeed mode selection
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this will enable small planes flying without an
airspeed sensor
2016-06-23 09:08:34 +02:00
1ecdb0f6fb
adjust stack sizes
2016-05-19 21:49:34 +02:00
76387b1693
uorb autogeneration
2016-05-14 11:27:07 +02:00
b471d94069
fw_att_control_params.c param metadata
2016-05-11 12:29:49 -04:00
901461f301
FW att ctrl: Reduce perf counters
2016-05-05 20:08:54 +02:00
41c1e56075
FW stabalized mode properly initialize att_sp
2016-04-23 15:50:43 +02:00
967e4dd127
Modified cmake to use STACK_MAX and STACK_MAIN
2016-04-14 13:36:36 -04:00
1f44fb1efd
commander: internalize system status bools
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Most condition bools in the commander are not used anywhere but in the
commander. It therefore makes sense to move them to a different internal
struct and remove them from the vehicle_status message.
Also, the land_detected should be used by all the modules instead of
getting it through the commander and system_status.
2016-04-11 18:01:47 +02:00
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
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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
CAI Dongcai