Semi-Analytical Midcourse Guidance for Coordinated Interception of Multiple Exo-Atmospheric Targets

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Guoxu Zhang, Bo Pang, Changxuan Wen, Xun Song
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引用次数: 0

Abstract

The simultaneous interception of multiple exo-atmospheric threat targets can leave no buffer time for the targets and greatly reduces targets’ penetration probability. This paper proposes centralized and decentralized two midcourse guidance methods to solve the coordinated interception of multiple exo-atmospheric targets. First, the free-time cooperative interception problem minimizing the total impulses is established, where the nonlinear dynamics of the interceptors and targets, the initial impulse constraints, and the terminal interception constraints are considered. Second, the necessary conditions for the optimal cooperative interception problem are derived and then approximated using higher-order Taylor expansions, which result in a series of analytical nonlinear equations. Then, the semi-analytical centralized guidance mode is designed to achieve simultaneous interception of targets by directly solving the analytical nonlinear equations. To improve computational efficiency, the decentralized cooperative guidance mode is further proposed by using the developed iterative freezing trajectory method, where each interceptor uses information from other interceptors in the previous iteration for prediction and distributed computation. Numerical examples verify the effectiveness and robustness of the proposed two guidance methods. Results show that the computational efficiency of the decentralized guidance mode is more efficient compared with the centralized midcourse guidance mode.
多个大气层外目标协同拦截的半解析中段制导
同时拦截多个大气层外威胁目标,不会给目标留下缓冲时间,大大降低了目标的突防概率。针对多个大气层外目标的协同拦截问题,提出了集中和分散两种中段制导方法。首先,建立了总脉冲最小化的自由时间协同拦截问题,其中考虑了拦截器和目标的非线性动力学、初始脉冲约束和终端拦截约束。其次,导出了最优协同拦截问题的必要条件,然后使用高阶泰勒展开进行近似,得到了一系列解析非线性方程。然后,设计了半解析集中制导模式,通过直接求解解析非线性方程组来实现对目标的同时拦截。为了提高计算效率,通过使用开发的迭代冻结轨迹方法,进一步提出了分散协同制导模式,其中每个拦截器在上一次迭代中使用来自其他拦截器的信息进行预测和分布式计算。数值算例验证了所提出的两种制导方法的有效性和鲁棒性。结果表明,与集中式中段制导模式相比,分散制导模式的计算效率更高。
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来源期刊
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
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