通过星光测量确定飞行器姿态的Kalman滤波估计

The Kalman Filtering Estimation of Determining a Spacecraft Attithde by Measuring Starlight

针对飞行器姿态控制问题引入星光测量方法,并对四元数方法的应用进行了详细讨论,给出了一种四元数最优估计算法。

To solve the problem of spacecraft attitude control,the starlight measurement method is introduced and the application of the quaternion method is discussed in detail so that a certain quaternion estimation algorithm is presented.