Tracking micro reentering USV with TDRS and ground stations using adaptive IMM method

Li-qiang Hou, Hengnian Li, Fu-Ming Huang, Pu Huang
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引用次数: 2

Abstract

In this paper, a tracking system with multi-sensors is presented, in which a sub-orbit USV (unmanned space vehicle) of wave-rider shape is tracked by a TDRS (Tracking and Data Relay Satellite) and ground stations. Because of high lift-drag ratio and maneuverability, the vehicle, once is used in reentering purpose, a complicated trajectory will be produced and cause big challenges for tracking facilities. Although TDRS has more coverage capability than ground stations, unlike tracking stations fixed on the ground, when its antenna tracks target, the platform it located on will do some attitude maneuver to balance the effects caused by the antenna's moving. This will lead some errors in tracking the target and should be taken into account when processing the data. To solve these problems, a fusion strategy of improved IMM (Interacting Multiple Model) with different kinematics and measurement models is designed in this paper, which helps to process the trajectory data and estimate aerodynamic parameters of the vehicle. In the dynamic model, both trajectory parameters and aerodynamics parameters are calculated, the measurement models are either TDRS or ground tracking stations. Meanwhile, in the adaptive IMM algorithm, an adaptive method for calculating transition probabilities of time-varying transition model is designed. Also the Iterated Sigma Point Kalman Filter (ISPKF) is used helping make the system more robust and perform better. Simulation results show that the proposed algorithm performs well in tracking high lift-drag ration re-entering vehicle and estimating the aerodynamics parameters as well.
基于自适应IMM方法的TDRS和地面站跟踪微型再入USV
本文提出了一种由跟踪与数据中继卫星(TDRS)和地面站对波浪形状的亚轨道无人飞行器(USV)进行多传感器跟踪的系统。由于高升阻比和高机动性,飞行器一旦用于再入,将产生复杂的轨迹,给跟踪设施带来很大的挑战。TDRS虽然具有比地面站更强的覆盖能力,但与固定在地面上的跟踪站不同,当其天线跟踪目标时,其所在平台会进行一定的姿态机动,以平衡天线移动带来的影响。这将导致跟踪目标时出现一些误差,在处理数据时应考虑到这一点。针对这些问题,本文设计了一种改进的多模型交互模型(IMM)与不同的运动学和测量模型的融合策略,有助于对飞行器的轨迹数据进行处理和气动参数估计。在动力学模型中,计算了弹道参数和空气动力学参数,测量模型为TDRS或地面跟踪站。同时,在自适应IMM算法中,设计了一种计算时变过渡模型转移概率的自适应方法。采用迭代西格玛点卡尔曼滤波(ISPKF),使系统具有更好的鲁棒性和性能。仿真结果表明,该算法在高升阻比再入飞行器跟踪和空气动力学参数估计方面具有良好的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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