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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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DSDL comments update
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@@ -1,6 +1,6 @@
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#
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# Generic actuator feedback, if available.
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# Unknown components should be NAN.
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# Unknown fields should be set to NAN.
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#
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uint8 actuator_id
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@@ -4,4 +4,12 @@
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#
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uint8 actuator_id
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float16 command # Any units. For a generic servo use [-1; 1].
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#
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# Recommended units are, either:
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# - Unitless [-1; 1]
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# - Angular position in radians
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# - Linear position in meters
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# Status report should normally use the same units.
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#
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float16 command
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@@ -1,5 +1,5 @@
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#
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# True airspeed.
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# True airspeed in meters per second.
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#
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float16 true_airspeed
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@@ -1,13 +1,12 @@
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#
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# Pressure altitude and barometric climb rate.
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# Barometer nodes should publish this message.
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# Pressure altitude in meters and barometric climb rate in meters per second.
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#
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uavcan.Timestamp timestamp
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float32 pressure_altitude
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float16 pressure_altitude_variance
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float32 pressure_altitude # m
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float16 pressure_altitude_variance # m^2
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# Positive if climbing up
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float16 climb_rate
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float16 climb_rate_variance
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float16 climb_rate # m/s
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float16 climb_rate_variance # m^2/s^2
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@@ -1,10 +1,10 @@
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#
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# Angle of attack.
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# Angle of attack in radians.
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#
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uint8 SENSOR_ID_LEFT = 254
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uint8 SENSOR_ID_RIGHT = 255
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uint8 sensor_id
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float16 aoa
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float16 aoa_variance
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float16 aoa # Radians
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float16 aoa_variance # Radians^2
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@@ -3,5 +3,5 @@
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# Yaw right: +, yaw left: -
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#
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float16 sideslip_angle
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float16 sideslip_angle_variance
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float16 sideslip_angle # Radians
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float16 sideslip_angle_variance # Radians^2
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@@ -1,7 +1,6 @@
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#
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# Raw ESC command.
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# Direct transition from disarmed state to high thrust should be rejected by the ESC.
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# Non-zero setpoint value below minimum should be interpreted as min valid setpoint.
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# Non-zero setpoint value below minimum should be interpreted as min valid setpoint for the given motor.
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# Negative values indicate reverse rotation.
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#
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@@ -1,12 +1,13 @@
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#
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# Generic ESC status.
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# Unknown fields should be set to NAN.
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#
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uint32 error_count # Since the motor started; normally should not overflow
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uint32 error_count # Resets when the motor restarts
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float16 voltage # Volt, NAN if unknown
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float16 current # Ampere, NAN if unknown. Can be negative in case of a regenerative braking.
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float16 temperature # Kelvin, NAN if unknown
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float16 voltage # Volt
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float16 current # Ampere. Can be negative in case of a regenerative braking.
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float16 temperature # Kelvin
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int18 rpm # Negative value indicates reverse rotation
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@@ -8,8 +8,8 @@ uint4 MODE_ORIENTATION_BODY_FRAME = 2
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uint4 MODE_GEO_POI = 3
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uint4 mode
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#
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# Camera axis orientation in body frame (not in fixed frame).
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# In case if the gimbal can only measure orientation relative to the fixed frame (e.g. using a dedicated IMU),
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# it shall transform the orientation into the body frame automatically.
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#
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float16[4] body_frame_orientation_xyzw
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float16[<=9] body_frame_orientation_covariance # +inf for non-existent axes
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@@ -1,6 +1,6 @@
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#
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# Nested type.
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# RGB color in 5-6-5 16-bit palette.
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# RGB color in the standard 5-6-5 16-bit palette.
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# Monocolor lights should interpret this as brightness setpoint: from zero (0, 0, 0) to full brightness (31, 63, 31).
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#
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@@ -1,6 +1,6 @@
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#
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# Nested type.
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# Controls single light source, color of monochrome.
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# Controls single light source, color or monochrome.
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#
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uint8 light_id
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@@ -1,5 +1,5 @@
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#
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# X/Y velocities estimated by simple downward looking optical flow sensor.
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# X/Y velocities estimated by a simple downward looking optical flow sensor.
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#
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uavcan.Timestamp timestamp
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@@ -1,6 +1,6 @@
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#
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# Altitude above ground level.
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# A single node can publish the measurements from different sensors concurrently.
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# A single node can publish measurements from different sensors concurrently.
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#
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uavcan.Timestamp timestamp
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