基于气动模型的高超声速滑翔飞行器雷达跟踪

Jingshuai Huang, Hong-bo Zhang, G. Tang, Weimin Bao
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引用次数: 2

摘要

为了在拦截高超声速滑翔飞行器方面实现击杀,首要任务是精确跟踪飞行状态和预测弹道。提出了一种基于新型气动模型的高超声速滑翔飞行器雷达跟踪方法。在已建立的气动加速度的基础上,导出了扩展运动方程,并给出了雷达的测量方程。针对非线性问题,分别采用扩展卡尔曼滤波器和无气味卡尔曼滤波器对扩展状态进行估计。为了验证所提出的方法,设计了两种类型的标准轨迹,然后进行了跟踪。仿真结果表明,该方法能够精确跟踪高超声速滑翔飞行器,为后续弹道预测提供了保证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Radar tracking for hypersonic glide vehicle based on aerodynamic model
In order to achieve hit-to-kill in terms of intercepting the hypersonic glide vehicle, the first task is to accurately track the flight state and predict the trajectory. In this paper, a radar tracking approach for hypersonic glide vehicles is proposed based on a novel aerodynamic model. The extended motion equations are derived on basis of the established aerodynamic acceleration, and the measurement equations of radar are given. In view of the nonlinearities, the extended and unscented Kalman filters are adopted to estimate the extended state, respectively. To examine the proposed method, two types of standard trajectories are designed and then tracked. Simulation results indicate that it can precisely track the hypersonic glide vehicle, which provides a guarantee of the following trajectory prediction.
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