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authorThomas Gubler <thomasgubler@gmail.com>2014-12-16 08:22:58 +0100
committerThomas Gubler <thomasgubler@gmail.com>2014-12-16 08:22:58 +0100
commit9980e4482146333340cc105b560bdbd26acb999f (patch)
tree45fa3a0660abf6e54daad393cf8f147d112e4b5c /msg/vehicle_attitude_setpoint.msg
parente38d0c27bdd56335ed002aa6b469dcadf90bf0dc (diff)
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moved msg files
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diff --git a/msg/vehicle_attitude_setpoint.msg b/msg/vehicle_attitude_setpoint.msg
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+
+uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
+
+float32 roll_body # body angle in NED frame
+float32 pitch_body # body angle in NED frame
+float32 yaw_body # body angle in NED frame
+
+float32[9] R_body # Rotation matrix describing the setpoint as rotation from the current body frame
+bool R_valid # Set to true if rotation matrix is valid
+
+# For quaternion-based attitude control
+float32[4] q_d # Desired quaternion for quaternion control
+bool q_d_valid # Set to true if quaternion vector is valid
+float32[4] q_e # Attitude error in quaternion
+bool q_e_valid # Set to true if quaternion error vector is valid
+
+float32 thrust # Thrust in Newton the power system should generate
+
+bool roll_reset_integral # Reset roll integral part (navigation logic change)
+bool pitch_reset_integral # Reset pitch integral part (navigation logic change)
+bool yaw_reset_integral # Reset yaw integral part (navigation logic change)