多飞行器再入段时间协同弹道规划方法

姜鹏; 郭栋; 韩亮; 李清东; 任章

doi:10.7527/S1000-6893.2019.23776

航空学报 >

2020 , Vol. 41 >Issue S1: 723776 - 723776

DOI: https://doi.org/10.7527/S1000-6893.2019.23776

多飞行器再入段时间协同弹道规划方法

姜鹏 ,
郭栋 ,
韩亮 ,
李清东 ,
任章

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1. 国防科技大学系统工程学院, 长沙 410073;
2. 中国运载火箭技术研究院, 北京 100076;
3. 北京航空航天大学自动化科学与电气工程学院, 北京 100083;
4. 北京航空航天大学中法工程师学院, 北京 100083;
5. 北京航空航天大学大数据科学与脑机智能高精尖创新中心, 北京 100083

收稿日期: 2019-12-13

修回日期: 2019-12-26

网络出版日期: 2020-01-02

基金资助

国家自然科学基金（61922008，61973013，61873011，61803014）

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Trajectory optimization for cooperative reentry of multiple hypersonic glide vehicle

JIANG Peng ,
GUO Dong ,
HAN Liang ,
LI Qingdong ,
REN Zhang

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1. College of Systems Engineering, National University of Defense Technology, Changsha 410073, China;
2. China Academy of Launch Vehicle Technology, Beijing 100076, China;
3. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China;
4. School of Sino-French Engineer, Beihang University, Beijing 100083, China;
5. Beijing Advanced Innovation Center for Big Data and Brain Computing, Beihang University, Beijing 100083, China

Received date: 2019-12-13

Revised date: 2019-12-26

Online published: 2020-01-02

Supported by

National Natural Science Foundation of China (61922008, 61973013, 61873011, 61803014)

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摘要

提出了一种多飞行器再入段时间协同弹道规划方法。首先，在纵向平面内规划满足航程与终端约束的纵向标称轨迹。随后，在采用轨迹跟踪律跟踪纵向标称轨迹的同时，运用考虑初始横侧向状态的多边界航向偏差角走廊策略控制飞行器的横侧向机动，以满足到达时间约束与终端约束，进而实现单枚飞行器到达时间约束下的轨迹规划。在此基础上，完成了飞行器的到达时间分布与飞行能力分析，给出了最小与最大到达时间的分析计算方法，并根据多飞行器协同再入的任务需求完成了协同飞行时间决策。最后，多飞行器协同再入与扰动条件下的仿真结果表明，该方法能够规划出满足到达时间与终端约束的协同再入轨迹，具备良好的计算精度与鲁棒性。

关键词： 弹道规划; 到达时间约束; 高超声速滑翔飞行器; 飞行走廊; 轨迹跟踪

本文引用格式

姜鹏 , 郭栋 , 韩亮 , 李清东 , 任章 . 多飞行器再入段时间协同弹道规划方法[J]. 航空学报, 2020 , 41(S1) : 723776 -723776 . DOI: 10.7527/S1000-6893.2019.23776

Abstract

This paper presents a trajectory optimization method for the cooperative reentry of multiple hypersonic glide vehicles. First, the nominal longitudinal trajectory is planned to satisfy the path and terminal constraints. Second, the trajectory tracking law is used to track the nominal longitudinal trajectory. Meanwhile, a multi-layer bounded corridor for heading error considering the initial lateral state is proposed to control the lateral maneuver, so as to meet the requirement of arrival time and the terminal constraints. Then the trajectory planning with arrival time constraints for a single vehicle is implemented. On this basis, the arrival time distribution and the flight capability are analyzed, and the analysis and the calculation methods for the minimum and the maximum arrival time are given. For the multiple hypersonic glide vehicle cooperative reentry scenario, the cooperative flight time decision-making is completed. Finally, numerical results show that the trajectory optimization method achieves a good performance on the arrival time and the terminal constraints, which indicates that the proposed method can realize the cooperative reentry of multiple hypersonic glide vehicle. The results in dispersed cases indicate that the trajectory optimization method has good calculation accuracy and robustness.

Key words： trajectory optimization; arrival time constraint; hypersonic glide vehicle; flight corridor; trajectory tracking

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