Zhang Hao, Niu Yanxiong, Lu Jiazhen, Zhang He
Appl Opt. 2016 Nov 20;55(33):9427-9434. doi: 10.1364/AO.55.009427.
Angular velocity information is a requisite for a spacecraft guidance, navigation, and control system. In this paper, an approach for angular velocity estimation based merely on star vector measurement with an improved current statistical model Kalman filter is proposed. High-precision angular velocity estimation can be achieved under dynamic conditions. The amount of calculation is also reduced compared to a Kalman filter. Different trajectories are simulated to test this approach, and experiments with real starry sky observation are implemented for further confirmation. The estimation accuracy is proved to be better than 10 rad/s under various conditions. Both the simulation and the experiment demonstrate that the described approach is effective and shows an excellent performance under both static and dynamic conditions.
角速度信息是航天器制导、导航与控制系统所必需的。本文提出了一种仅基于星矢量测量,采用改进的当前统计模型卡尔曼滤波器进行角速度估计的方法。在动态条件下可实现高精度的角速度估计。与卡尔曼滤波器相比,计算量也有所减少。模拟了不同轨迹以测试该方法,并进行了真实星空观测实验以进一步验证。结果证明,在各种条件下估计精度均优于10 rad/s。仿真和实验均表明,所描述的方法是有效的,并且在静态和动态条件下均表现出优异的性能。