Merge px4 1.13.2 #4
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Signed-off-by: Silvan Fuhrer <[email protected]>
Weather vane should only set a yawrate setpoint, but no yaw setpoint. Setting it to NAN when WV is active makes sure that whatever _yaw_setpoint is set previously (e.g. through Waypoint) is not used. Signed-off-by: Silvan Fuhrer <[email protected]>
…e_control message
- on some H7 boards (cuav x7pro tested) there's an occasional hard fault when starting the mavlink shell that is no longer reproducible with the slightly expanded locking - this is likely just changing the timing (holding the sched lock for longer), but this should be harmless for now until we can identify the root cause
when the vertical pos or vel innov ratio is above the threshold, the other one needs to be significant too and not just positive to trigger the failure
- remove drv_airspeed.h and ioctls
… and cleanup - split ms4525_airspeed into separate ms4515 and ms4525 drivers
…4#19539) Co-authored-by: chris1seto <[email protected]> Co-authored-by: chris1seto <[email protected]>
add V5X004002
My assumption is that the bus are numbered < 127. This saves about 100 bytes of flash.
As I understand it, only Rev 1 and Rev 2 were shipped by HB, and likely to be used for the Mini and CM4.
As I understand it, only Rev 3 and Rev 4 were shipped by HB for Mini and CM4, and are likely to be used for it. It would be nice to have all combinations but it requires quite some flash in the current implementation.
- Removed commented out config data. - hw_mft_list_v0540 was the same as hw_mft_list_v0500
- alias from hw_mft_list_v0650 to hw_mft_list_v0600 as it is the same - add V6X50 again
This fixes the errors showing up at startup for me with a Black Cube.
This was forgotton with all the merges and shuffling previously.
This fixes a Python 3.10 issue for me.
Before this fix, this function would stall and somehow never return.
Clear the calibration at the end only otherwise everything gets erased at the end of the first iteration of the outer loop
This prevents publishing a negative pressure which leads to a NAN altitude estimate further down the line.
- vehicle_imu_status can publish immediately on any measured sample rate change or sensor error increment, but the windowed mean/variance shouldn't necessarily reset that often
…ator::Navigator() This fixes the issue where the init happended in the initializer list, at which point the params were not yet initialized and thus resulted in random values for the init values of _mission_item.loiter_radius and .acceptance_radius. Signed-off-by: Silvan Fuhrer <[email protected]>
…ight mag cal - preflight mag bias estimate is in the vehicle body frame and removed from the raw mag data after it's rotated, calibrated, etc - in flight mag bias (from ekf2) is in the vehicle body frame, but stored as a sensor frame offset immediately
to avoid float rounding errors leading to tiny acceptance radii getting considered
…r takeoff items otherwise a previously adjusted or uninitialized radius from the last flight can cause problems during the new takeoff
Signed-off-by: Julian Oes <[email protected]>
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@hardikparwana whenever you are done with RSS, lets talk about making this our main branch. |
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This branch works, and it has been updated with the px4 v1.13.2
I propose we replace current
masterwith this branchit has been tested in sim and in experiments on a quad.
probably worth checking if this still works on a rover before.