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9 lines
503 B
9 lines
503 B
uint64 timestamp # time since system start (microseconds) |
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float32 roll # body angular rates in NED frame |
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float32 pitch # body angular rates in NED frame |
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float32 yaw # body angular rates in NED frame |
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# For clarification: For multicopters thrust_body[0] and thrust[1] are usually 0 and thrust[2] is the negative throttle demand. |
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# For fixed wings thrust_x is the throttle demand and thrust_y, thrust_z will usually be zero. |
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float32[3] thrust_body # Normalized thrust command in body NED frame [-1,1]
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