- move posix-configs/SITL/init/{rcS,10016_iris,6011_typhoon_h480} to ROMFS/px4fmu_common/init.d-posix
allows for easier unification, only one symlink is required.
- rcS: add AUTOCNF support. Update scripts to match with behavior of PX4
master (parameter values, some sitl driver got removed)
- add alias to allow 'set variable value' syntax in scripts to px4-alias.sh
- use px4_getopt
- use separate argument for the test_data directory
- append PATH from within the px4 binary: this simplifies the usage
w/o the sitl_run.sh script.
- add 'source px4-alias.sh' to all existing sitl startup scripts
- move sitl mixers to ROMFS/px4fmu_common/mixers-sitl
makes it easier to use existing mixers and sitl-specific ones.
- remove unused rcS_gazebo_delta_wing
- use mixer for the simulation to the sitl mixer dir
- do not use virtual elevator in the mixer for the real vehicle
Signed-off-by: Roman <bapstroman@gmail.com>
* Lists ROMFS files explicity instead of using GLOB_RECURSE
Previously, when ROMFS files that were not airframes were touched, the ROMFS
would not be rebuilt. The ROMFS files are now specified explicityl in a
CMakeLists.txt file that is located in the root ROMFS directory.
Now when one of the ROMFS files is touched the whole ROMFS is rebuilt.
When new files are added to the ROMFS, they need to be explicity added to
the CMakeLists in the ROMFS root directory.
* ROMFS: adds individual CMakeLists files in each subdirectory
Also moves the temporary ROMFS build directory to ${PX4_BINARY_DIR}/ROMFS/genromfs
so that the cmake_install.cmake files and the CMakeFiles directories (generated whenever
are not add_subdirectory() is called) are not generated in the temporary ROMFS directory
from which the ROMFS binary is created.
* cmake ROMFS generate add px4_add_romfs_files function
* ROMFS CMakeLists: adds explanatory comment to px4_add_romfs_files function
* ROMFS CMakeLists: updates copyright headers
- simulated tailsitter needs a virtual elevator since we cannot simulate
elevons yet (liftDrag plugin does not model longitudinal moment Cm)
Signed-off-by: Roman <bapstroman@gmail.com>
It makes sense to have this for all standard planes and our default PWM outputs for MAIN are always 6 wide, so this should scale to all known HW platforms.
* UAVCAN ESC output: removing ESC output channels from published message that are always zero. This allows the UAVCAN stack to always transfer only the minimum number of output values, avoiding redundant zeroes and the associated increase in bus load and CPU time
* Added a separate mixer file for CAN quadrotor
* Sampling profiler improvements
* PMSP: Output more endpoints
* Matrix update
* libc usage workaround
* Removed UAVCAN perfcounters
* Matrix submodule update
* UAVCAN ESC output: removing ESC output channels from published message that are always zero. This allows the UAVCAN stack to always transfer only the minimum number of output values, avoiding redundant zeroes and the associated increase in bus load and CPU time
* Added a separate mixer file for CAN quadrotor
* Sampling profiler improvements
* PMSP: Output more endpoints
* Matrix update
* libc usage workaround
* Removed UAVCAN perfcounters
MavLink spec implementation
implemented vehicle_roi topic
rename old gimbal to rc_gimbal
little changes
corrected RC Gimbal group
Starting ROI implementation in commander
implementation done, needs to be tested
uhm..
add todo
Change to float32 for x,y and z
remove mission topic again, not needed
change roi coordinates to lat, lon and alt
adjust to float64
starting mount implementation
correcting small mistakes, compiles now
add todos
further progress
implementing parameters
adjust default parameters
started implementation of mavlink
fix typo
change to lat, lon and alt
fix typo :D
change to double (to represent float64)
add global_position_
add mount topic
commander mount implementation done
cleanup
almost finished
little fix
codestyle fixes
leave pitch at 0 degrees
added pitch calculation
codestyle changes
Undo vehicle_mount, react to updated parameters, parsing of CMD_DO_MOUNT_* in mount.cpp
start implementing mode override
forgot a semikolon.
add debug
Finish implementation of mount override and manual control.
fix codestyle
correct cleanup
rename to vmount
works now
fix rebase error
fix polling
refactoring and custom airframe for gimbal
couple changes
remove warnx
almost done
finally
What is going on?
change back to actuator_controls_2
working
bump parameter version number and some clarification
fix submodules
* Helicopter aiframe and basic PID control
* codestyle
* Blade 130x gains working but not optimal
* Changed behaviour of feedforward for all multicopter
Beat Küng