Arquivos
ardrone_autonomy/ARDroneLib/Soft/Lib/Maths/quaternions.c
T
2012-06-26 12:19:39 -07:00

143 linhas
3.5 KiB
C

/**
* \file quaternions.c
* \brief Quaternions library used by Mykonos
* \author Francois Callou <francois.callou@parrot.com>
* \version 1.0
*/
#include <VP_Os/vp_os_assert.h>
#include <Maths/quaternions.h>
#include <Maths/maths.h>
const quaternion_t quat_unitary = { 1.0f, {{{ 0.0f, 0.0f, 0.0f}}} };
void mul_quat( quaternion_t* out, quaternion_t* q1, quaternion_t* q2)
{
vector31_t temp_v;
/// You can't have output & input pointing to the same location
VP_OS_ASSERT( out != q1 );
VP_OS_ASSERT( out != q2 );
// scalar result
out->a = q1->a*q2->a - (q1->v.x*q2->v.x + q1->v.y*q2->v.y + q1->v.z*q2->v.z);
// pure quaternion result
cross_vec( &out->v , &q1->v, &q2->v );
mulconst_vec( &temp_v, &q2->v, q1->a );
add_vec( &out->v, &out->v, &temp_v);
mulconst_vec( &temp_v, &q1->v, q2->a );
add_vec( &out->v, &out->v, &temp_v);
}
void add_quat( quaternion_t* out, quaternion_t* q1, quaternion_t* q2 )
{
// scalar result
out->a = q1->a + q2->a;
// pure quaternion result
add_vec( &out->v, &q1->v, &q2->v );
}
void mulconst_quat( quaternion_t* out, quaternion_t* q, float32_t k )
{
out->a = (q->a) * k;
mulconst_vec( &out->v, &q->v, k );
}
void conjugate_quat( quaternion_t* out, quaternion_t* q )
{
out->a = q->a;
out->v.x = -q->v.x;
out->v.y = -q->v.y;
out->v.z = -q->v.z;
}
float32_t norm_quat( quaternion_t *q )
{
return sqrtf( q->a*q->a + q->v.x * q->v.x + q->v.y * q->v.y + q->v.z * q->v.z );
}
bool_t normalize_quat( quaternion_t* q )
{
bool_t ret;
float32_t norm;
norm = norm_quat( q );
if( f_is_zero( norm ) )
{
q->a = 0.0f;
q->v.x = 0.0f;
q->v.y = 0.0f;
q->v.z = 0.0f;
ret = FALSE;
}
else
{
q->a = f_zero( q->a / norm );
q->v.x = f_zero( q->v.x / norm );
q->v.y = f_zero( q->v.y / norm );
q->v.z = f_zero( q->v.z / norm );
ret = TRUE;
}
return ret;
}
void quat_to_euler_rot_mat(matrix33_t* m, quaternion_t* q)
{
//to use with normalised quaternion
m->m11 = 1.0f - 2*q->v.y*q->v.y - 2*q->v.z*q->v.z;
m->m12 = 2*q->v.x*q->v.y - 2*q->v.z*q->a;
m->m13 = 2*q->v.z*q->v.x + 2*q->v.y*q->a;
m->m21 = 2*q->v.x*q->v.y + 2*q->v.z*q->a;
m->m22 = 1.0f - 2*q->v.x*q->v.x - 2*q->v.z*q->v.z;
m->m23 = 2*q->v.z*q->v.y - 2*q->v.x*q->a;
m->m31 = 2*q->v.z*q->v.x - 2*q->v.y*q->a;
m->m32 = 2*q->v.z*q->v.y + 2*q->v.x*q->a;
m->m33 = 1.0f - 2*q->v.x*q->v.x - 2*q->v.y*q->v.y;
}
void quat_to_euler_angles(angles_t* a, quaternion_t* q)
{
//to use with normalised quaternion
float32_t sqvx = q->v.x*q->v.x;
float32_t sqvy = q->v.y*q->v.y;
float32_t sqvz = q->v.z*q->v.z;
/* if ( f_is_zero(test -0.5) ) { // singularity at north pole
a->psi = 2 * atan2(q->a,q->v.z);
a->theta = PI/2;
a->phi = 0;
return;
}
if ( f_is_zero(test + 0.5) ) { // singularity at south pole
a->psi = -2 * atan2(q->a,q->v.z);
a->theta = - PI/2;
a->phi = 0;
return;
}*/
a->phi = atan2f(2*q->v.y*q->v.z+2*q->a*q->v.x , 1 - 2*sqvx - 2*sqvy);
a->theta = asinf(2*(q->a*q->v.y - q->v.x*q->v.z ));
a->psi = atan2f(2*q->v.x*q->v.y+2*q->a*q->v.z , 1 - 2*sqvy - 2*sqvz);
}
void euler_angles_to_quat(angles_t* a, quaternion_t* q)
{
float32_t cphi_2, sphi_2, cthe_2, sthe_2, cpsi_2, spsi_2;
sincosf((a->phi)*0.5f, &sphi_2, &cphi_2);
sincosf((a->theta)*0.5f, &sthe_2, &cthe_2);
sincosf((a->psi)*0.5f, &spsi_2, &cpsi_2);
q->a = cphi_2*cthe_2*cpsi_2 + sphi_2*sthe_2*spsi_2;
q->v.x = sphi_2*cthe_2*cpsi_2 - cphi_2*sthe_2*spsi_2;
q->v.y = cphi_2*sthe_2*cpsi_2 + sphi_2*cthe_2*spsi_2;
q->v.z = cphi_2*cthe_2*spsi_2 - sphi_2*sthe_2*cpsi_2;
}