mavlink v0.7.0 APM.Message.AttitudeQuaternionCov View Source
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t()
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t()
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t() :: %APM.Message.AttitudeQuaternionCov{
covariance: [Float32],
pitchspeed: Float32,
q: [Float32],
rollspeed: Float32,
time_usec: MAVLink.Types.uint64_t(),
yawspeed: Float32
}
t() :: %APM.Message.AttitudeQuaternionCov{ covariance: [Float32], pitchspeed: Float32, q: [Float32], rollspeed: Float32, time_usec: MAVLink.Types.uint64_t(), yawspeed: Float32 }
The attitude in the aeronautical frame (right-handed, Z-down, X-front, Y-right), expressed as quaternion. Quaternion order is w, x, y, z and a zero rotation would be expressed as (1 0 0 0).