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