@inproceedings{8f12c6dcc6be422aba8c8fe6fd3f84b2,
title = "Guidance Method for Re-Entry Glide Vehicle Considering No-Fly Zone Avoidance",
abstract = "In order to solve the problem of trajectory oscillation in the no-fly zone of the re-entry glide vehicle, the nominal trajectory is designed based on the quasi-equilibrium gliding conditions. The nominal trajectory is tracked based on the sliding mode control to ensure that the no-fly zone is avoided without deviating from the target point. A dynamic heading corridor design algorithm based on the improved artificial potential field method is proposed to determine the tilt inversion symbol. The results show that the proposed guidance algorithm can achieve quasi-equilibrium gliding in the longitudinal direction and avoid the no-fly zone in the lateral direction.",
keywords = "Improved artificial potential field, No-fly zone avoidance, Profile guidance, Re-entry gliding, Sliding mode control",
author = "Jing Hu and Weibo Sun and Mingyang Zhang and Tao Chao and Ming Yang",
note = "Publisher Copyright: {\textcopyright} 2023 Technical Committee on Control Theory, Chinese Association of Automation.; 42nd Chinese Control Conference, CCC 2023 ; Conference date: 24-07-2023 Through 26-07-2023",
year = "2023",
doi = "10.23919/CCC58697.2023.10240299",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3520--3525",
booktitle = "2023 42nd Chinese Control Conference, CCC 2023",
address = "美国",
}