Trajectory optimization for cooperative reentry of multiple hypersonic glide vehicle

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

doi:10.7527/S1000-6893.2019.23776

ACTA AERONAUTICAET ASTRONAUTICA SINICA >

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

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

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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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

Cite this article

JIANG Peng , GUO Dong , HAN Liang , LI Qingdong , REN Zhang . Trajectory optimization for cooperative reentry of multiple hypersonic glide vehicle[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020 , 41(S1) : 723776 -723776 . DOI: 10.7527/S1000-6893.2019.23776

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