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| void | CovariancePrediction (float F[NUMX][NUMX], float G[NUMX][NUMW], float Q[NUMW], float dT, float P[NUMX][NUMX]) |
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| void | SerialUpdate (float H[NUMV][NUMX], float R[NUMV], float Z[NUMV], float Y[NUMV], float P[NUMX][NUMX], float X[NUMX], uint16_t SensorsUsed) |
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| void | RungeKutta (float X[NUMX], float U[NUMU], float dT) |
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| void | StateEq (float X[NUMX], float U[NUMU], float Xdot[NUMX]) |
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| void | LinearizeFG (float X[NUMX], float U[NUMU], float F[NUMX][NUMX], float G[NUMX][NUMW]) |
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| void | MeasurementEq (float X[NUMX], float Be[3], float Y[NUMV]) |
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| void | LinearizeH (float X[NUMX], float Be[3], float H[NUMV][NUMX]) |
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| uint16_t | ins_get_num_states () |
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| void | INSGPSInit () |
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| void | INSSetArmed (bool armed) |
| | Set the current flight state. More...
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| void | INSGetState (float *pos, float *vel, float *attitude, float *gyro_bias, float *accel_bias) |
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| void | INSGetVariance (float *var_out) |
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| void | INSResetP (const float *PDiag) |
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| void | INSSetState (const float pos[3], const float vel[3], const float q[4], const float gyro_bias[3], const float accel_bias[3]) |
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| void | INSPosVelReset (const float pos[3], const float vel[3]) |
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| void | INSSetPosVelVar (float PosVar, float VelVar, float VertPosVar) |
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| void | INSSetGyroBias (const float gyro_bias[3]) |
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| void | INSSetAccelBias (const float accel_bias[3]) |
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| void | INSSetAccelVar (const float accel_var[3]) |
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| void | INSSetGyroVar (const float gyro_var[3]) |
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| void | INSSetMagVar (const float scaled_mag_var[3]) |
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| void | INSSetBaroVar (const float baro_var) |
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| void | INSSetMagNorth (const float B[3]) |
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| void | INSStatePrediction (const float gyro_data[3], const float accel_data[3], float dT) |
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| void | INSCovariancePrediction (float dT) |
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| void | INSCorrection (const float mag_data[3], const float Pos[3], const float Vel[3], float BaroAlt, uint16_t SensorsUsed) |
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