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Rework flaps/spoilers logic
- remove deprecated actuator_controls[INDEX_FLAPS/SPOILERS/AIRBRAKES] - use new topic normalized_unsigned_setpoint.msg (with instances flaps_setpoint and spoilers_setpoint) to pass into control allocation - remove flaps/spoiler related fields from attitude_setpoint topic - CA: add possibility to map flaps/spoilers to any control surface - move flaps/spoiler pitch trimming to CA (previously called DTRIM_FLAPS/SPOILER) - move manual flaps/spoiler handling from rate to attitude controller FW Position controller: change how negative switch readings are intepreted for flaps/spoilers (considered negative as 0). VTOL: Rework spoiler publishing in hover - pushlish spoiler_setpoint.msg in the VTOL module if in hover - also set spoilers to land configuration if in Descend mode Allocation: add slew rate limit of 0.5 to flaps/spoilers configuration change Instead of doing the flaps/spoilers slew rate limiting in the FW Position Controller (which then only is applied in Auto flight), do it consistently over all flight modes, so also for manual modes. Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@@ -5,9 +5,6 @@ uint8 INDEX_ROLL = 0
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uint8 INDEX_PITCH = 1
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uint8 INDEX_YAW = 2
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uint8 INDEX_THROTTLE = 3
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uint8 INDEX_FLAPS = 4
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uint8 INDEX_SPOILERS = 5
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uint8 INDEX_AIRBRAKES = 6
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uint8 INDEX_GIMBAL_SHUTTER = 3
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uint8 INDEX_CAMERA_ZOOM = 4
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@@ -128,6 +128,7 @@ set(msg_files
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MountOrientation.msg
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ModeCompleted.msg
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NavigatorMissionItem.msg
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NormalizedUnsignedSetpoint.msg
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NpfgStatus.msg
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ObstacleDistance.msg
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OffboardControlMode.msg
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@@ -26,7 +26,7 @@ float32 pitch # move forward, negative pitch rotation, nose down
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float32 yaw # positive yaw rotation, clockwise when seen top down
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float32 throttle # move up, positive thrust, -1 is minimum available 0% or -100% +1 is 100% thrust
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float32 flaps # flap position
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float32 flaps # position of flaps switch/knob/lever [-1, 1]
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float32 aux1
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float32 aux2
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@@ -0,0 +1,5 @@
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uint64 timestamp # time since system start (microseconds)
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float32 normalized_setpoint # [0, 1]
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# TOPICS flaps_setpoint spoilers_setpoint
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@@ -17,14 +17,4 @@ bool reset_integral # Reset roll/pitch/yaw integrals (navigation logic change)
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bool fw_control_yaw_wheel # control heading with steering wheel (used for auto takeoff on runway)
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uint8 apply_flaps # flap config specifier
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uint8 FLAPS_OFF = 0 # no flaps
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uint8 FLAPS_LAND = 1 # landing config flaps
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uint8 FLAPS_TAKEOFF = 2 # take-off config flaps
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uint8 apply_spoilers # spoiler config specifier
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uint8 SPOILERS_OFF = 0 # no spoilers
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uint8 SPOILERS_LAND = 1 # landing config spoiler
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uint8 SPOILERS_DESCEND = 2 # descend config spoiler
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# TOPICS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
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