PX4 Firmware
PX4 Autopilot Software http://px4.io
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Variables | |
float | SG [3] = sq(_state.quat_nominal(0)) - sq(_state.quat_nominal(1)) - sq(_state.quat_nominal(2)) + sq(_state.quat_nominal(3)) |
float | SQ [4] = 0.5f * ((_state.quat_nominal(1)*SG[0]) - (_state.quat_nominal(0)*SG[2]) + (_state.quat_nominal(3)*SG[1])) |
const float | daYawVar = TBD |
P [0][0] = yaw_variance*sq(SQ[2]) | |
const float daYawVar = TBD |
Definition at line 23 of file YawCovariance.c.
P[3][2] = yaw_variance*sq(SQ[2]) |
Definition at line 27 of file YawCovariance.c.
SG[2] = sq(_state.quat_nominal(0)) - sq(_state.quat_nominal(1)) - sq(_state.quat_nominal(2)) + sq(_state.quat_nominal(3)) |
Definition at line 11 of file YawCovariance.c.
Referenced by Ekf::increaseQuatYawErrVariance(), and Ekf::predictCovariance().
SQ[3] = 0.5f * ((_state.quat_nominal(1)*SG[0]) - (_state.quat_nominal(0)*SG[2]) + (_state.quat_nominal(3)*SG[1])) |
Definition at line 16 of file YawCovariance.c.
Referenced by Ekf::increaseQuatYawErrVariance(), and Ekf::predictCovariance().