The mode executor can run land mode which updates the home position to the landing location. This
can be not the desirable behavior and the home position should stay at the original location.
A flag is added to the configuration overrides to control if the home position is updated or not.
Some modes should only be run within the context of a mode executor and the user should not be able
to select them in the GCS. With this change, the external component registration request can be
used to set if a mode is selectable or not.
The simulated attitude can disturb the gimbal estimator and lead to strange behavior of the gimbal. So, since the hardware is not moving in HIL/SIH, we fake a static attitude towards the gimbal.
The update function of InputMavlinkGimbalV2 returns UpdatedNotActive when receiving control commands from a system or component that doesn't match the primary control. This can happen if a component just sends commands without being in control or when transitioning to a different primary control.
If the input is marked as already_active, it will reset last_input_active which in turn resets the primary control in the next iteration. According to the MAVLink gimbal protocol v2, a component needs to send MAV_CMD_DO_GIMBAL_MANAGER_CONFIGURE to start controlling the gimbal and to remove control. However, with the current implementation there are several other commands that would reset the primary control.
With this PR, the primary control remains with the component that requested it last if updates from a not active component are received.
The CameraFeedback module used only the vehicle attitude for the camera orientation so far. With this change, the gimbal_device_attitude_status is used to compute the global camera orientation when a gimbal is used.
If the capture GPIO is exposed to a signal with high frequency changes, a lot of
interrupts are scheduled and the handling of these call can worst-case
starve flight critical processes leading to a loss of control. Since camera capture
is not flight critical, we now give up the capture
functionality and stop the interrupts to prevent the starvation of other processes.
If the PPS GPIO is exposed to a signal with high frequency changes, a lot of
interrupts are scheduled and the handling of these calls can worst-case
starve flight critical processes leading to a loss of
control. Since PPS is not flight critical, we now give up the PPS
functionality and stop the interrupts to prevent the starvation of other processes.
The existing implementation has about 100ms difference to a reference clock. With the changes this error less than 25us.
- Use sensor_gps messages with hrt timestamps as RTC reference and not the system realtime clock. The PPS interrupt can then be aligned with the GPS clock system.
- Keep fallback based on system RTC when no PPS pulse was captured
- camera_trigger module always publishes the camera_trigger msg (independent of the camera feedback)
- Use camera_trigger msg and set the feedback flag
- Subscribing modules determine if the message is relevant based on the feedback message
When using an FMU channel as PPS capture GPIO, the rtc_edge_time is now set as well. The delay between actual capture and callback is compensated with the elapsed time of the rtc clock.
This PR changes the COM_ARM_MAG_STR parameter to accept values. If the parameter is set to 2, the check is performed and a warning is logged but the vehicle can still arm.
statfs accesses the file-system and can be blocking for an extended period. Since the SD card check is part of the preflight checks in the main thread of commander, it could block its execution and cause various issues. The SD card is only mounted in rcS during boot so the state will not change after the first check.
Michael Schaeuble