A Real-time Adaptive Filtering Algorithm for Reentry Maneuvering

Peng Dan, Tao Xi, Dan Wang
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Abstract

In order to solve the problem of the real-time reconstruction of the reentry trajectory with lift-to-drag controlling law during the spacecraft’s reentry flight, an adaptive UKF filtering algorithm was proposed by using external measurements and considering the actual engineering situations. The filter’s state model and observation model were given, and some adaptive processing methods were used, including the maneuver detection and model switching method, and the acceleration compensation method, which were used to deal with the real-time tracking of the maneuvering process of the return flight. The simulation results show that the proposed calculation method is feasible, and the proposed adaptive processing algorithm applying the acceleration compensation can do the robust estimation processing of the reentry trajectory. The research results have certain reference value for the real-time estimation of maneuvering reentry spacecraft.
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一种再入机动的实时自适应滤波算法
为了解决航天器在再入飞行过程中具有升阻控制律的再入轨迹实时重建问题,结合实际工程情况,利用外部测量数据,提出了一种自适应UKF滤波算法。给出了滤波器的状态模型和观测模型,并采用机动检测和模型切换法、加速度补偿法等自适应处理方法对返航机动过程进行实时跟踪。仿真结果表明,所提出的计算方法是可行的,采用加速度补偿的自适应处理算法能够对再入弹道进行鲁棒估计处理。研究结果对机动再入航天器的实时估计具有一定的参考价值。
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