中文说明:
飞机姿态角控制时,基于四元数和欧拉角的位置坐标转换关系,欧拉角控制法同四元数控制方法间的相互转换。
English Description:
Airplane attitude Angle control, based on the location of the quaternion and euler Angle coordinate transformation relations, euler Angle control with mutual transformation between quaternion method.