After smoothing the linera velocity setpoint, the EKF has trouble initializing, becuase the acceleration is too smooth, to combat this issue, there is a 1 second delay when initializing the mission mode
Instead of directly setting the attitude setpoint for usage inside the same module
only publish it to the uorb topic, which is subscribed to in the same module.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* battery: make time remaining estimation dependent on level flight characteristis for FW
* battery: fix that FW flight is also correctly detected when vehicle_status is not updated
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* FixedwingPositionControl: Move constant to header file
* flight phase estimation: use tecs height rate reference to check for level flight
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
When the CPU load monitor is started while already running, then the
idle thread last_times[0] is reset to the last 1 second, rather than
since when the CPU load monitor was last started. The remaining threads
are not impacted, since their last_times[i] is reset to zero here.
This results in the idle thread having a lower than real CPU load, with
the remaining CPU time being wrongly attributed as scheduler load.
* avoid waypoint following during backtransition
- if vehicle overshoots transition, make controller track the prev/current
waypoint line, this avoids large banking maneuvers that delay the transition further
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* navigator: use SETPOINT_TYPE_LAND as setpoint type for VTOL_LAND waypoints
such that fixed wing position controller can distinguish from other types
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* FixedWingPositionControl: split vtol backtransition logic into separate method
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* review changes
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* prevent loiter when approaching vtol backtransition and invalidate previous waypoint during mission landing
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* removed unused parameter
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* small renaming of transition mode
Signed-off-by: RomanBapst <bapstroman@gmail.com>
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Signed-off-by: RomanBapst <bapstroman@gmail.com>
When a state stops to be estimated it becomes a "consider state". Its value and variance are frozen but its covariance with other states continue to evolve normally.
- removes conservative accel bias variance limiting
- force symmetry is skipped after fusion of NED vel/pos (a direct measurement)
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Co-authored-by: bresch <brescianimathieu@gmail.com>
