C:/Documents and Settings/gw/My Documents/Other projects/flightos/Libraries/DCM.h File Reference

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Defines
#define	Kp_YAW   1.2
#define	Ki_YAW   0.00002
#define	OUTPUTMODE   1
Functions
void	DCM_reference (void)
void	Normalize (void)
void	Drift_correction (void)
void	Matrix_update (void)
void	Euler_angles (void)
Variables
float	DCM_Matrix [3][3]
float	Update_Matrix [3][3] = {{0,1,2},{3,4,5},{6,7,8}}
float	Temporary_Matrix [3][3]
float	Omega_Vector [3] = {0,0,0}
float	Omega_P [3] = {0,0,0}
float	Omega_I [3] = {0,0,0}
float	Omega [3] = {0,0,0}
float	errorRollPitch [3] = {0,0,0}
float	errorYaw [3] = {0,0,0}

---

Define Documentation

#define Ki_YAW   0.00002

#define Kp_YAW   1.2

#define OUTPUTMODE   1

---

Function Documentation

void DCM_reference

(

void

)

void Drift_correction

(

void

)

void Euler_angles

(

void

)

void Matrix_update

(

void

)

void Normalize

(

void

)

---

Variable Documentation

float DCM_Matrix[3][3]

Initial value:

 {
  {
    1,0,0  }
  ,{
    0,1,0  }
  ,{
    0,0,1  }
}

float errorRollPitch[3] = {0,0,0}

float errorYaw[3] = {0,0,0}

float Omega[3] = {0,0,0}

float Omega_I[3] = {0,0,0}

float Omega_P[3] = {0,0,0}

float Omega_Vector[3] = {0,0,0}

float Temporary_Matrix[3][3]

Initial value:

{
  {
    0,0,0  }
  ,{
    0,0,0  }
  ,{
    0,0,0  }
}

float Update_Matrix[3][3] = {{0,1,2},{3,4,5},{6,7,8}}