Apollo 10.0
自动驾驶开放平台
apollo::localization::msf::math结构体 参考

#include <math_util.h>

apollo::localization::msf::math 的协作图:

静态 Public 成员函数

static void EulerToQuaternion (const double x_euler, const double y_euler, const double z_euler, double qbn[4])
 
static void QuaternionToDcm (const double *quaternion, double dcm[3][3])
 

详细描述

在文件 math_util.h26 行定义.

成员函数说明

◆ EulerToQuaternion()

static void apollo::localization::msf::math::EulerToQuaternion ( const double  x_euler,
const double  y_euler,
const double  z_euler,
double  qbn[4] 
)
inlinestatic

在文件 math_util.h27 行定义.

28 {
29 qbn[0] = sin(x_euler / 2.0) * sin(y_euler / 2.0) * sin(z_euler / 2.0) +
30 cos(x_euler / 2.0) * cos(y_euler / 2.0) * cos(z_euler / 2.0);
31 qbn[1] = cos(y_euler / 2.0) * cos(z_euler / 2.0) * sin(x_euler / 2.0) +
32 cos(x_euler / 2.0) * sin(y_euler / 2.0) * sin(z_euler / 2.0);
33 qbn[2] = cos(x_euler / 2.0) * cos(z_euler / 2.0) * sin(y_euler / 2.0) -
34 cos(y_euler / 2.0) * sin(x_euler / 2.0) * sin(z_euler / 2.0);
35 qbn[3] = cos(z_euler / 2.0) * sin(x_euler / 2.0) * sin(y_euler / 2.0) -
36 cos(x_euler / 2.0) * cos(y_euler / 2.0) * sin(z_euler / 2.0);
37
38 return;
39 }
float cos(Angle16 a)
Definition angle.cc:42
float sin(Angle16 a)
Definition angle.cc:25

◆ QuaternionToDcm()

static void apollo::localization::msf::math::QuaternionToDcm ( const double *  quaternion,
double  dcm[3][3] 
)
inlinestatic

在文件 math_util.h41 行定义.

41 {
42 dcm[0][0] = quaternion[0] * quaternion[0] + quaternion[1] * quaternion[1] -
43 quaternion[2] * quaternion[2] - quaternion[3] * quaternion[3];
44 dcm[0][1] =
45 2 * (quaternion[1] * quaternion[2] - quaternion[0] * quaternion[3]);
46 dcm[0][2] =
47 2 * (quaternion[1] * quaternion[3] + quaternion[0] * quaternion[2]);
48
49 dcm[1][0] =
50 2 * (quaternion[1] * quaternion[2] + quaternion[0] * quaternion[3]);
51 dcm[1][1] = quaternion[0] * quaternion[0] - quaternion[1] * quaternion[1] +
52 quaternion[2] * quaternion[2] - quaternion[3] * quaternion[3];
53 dcm[1][2] =
54 2 * (quaternion[2] * quaternion[3] - quaternion[0] * quaternion[1]);
55
56 dcm[2][0] =
57 2 * (quaternion[1] * quaternion[3] - quaternion[0] * quaternion[2]);
58 dcm[2][1] =
59 2 * (quaternion[2] * quaternion[3] + quaternion[0] * quaternion[1]);
60 dcm[2][2] = quaternion[0] * quaternion[0] - quaternion[1] * quaternion[1] -
61 quaternion[2] * quaternion[2] + quaternion[3] * quaternion[3];
62 return;
63 }

该结构体的文档由以下文件生成: