TY - GEN
T1 - Guidance Strategy for Hypersonic Glide Vehicle with Additional Angular Error Approach
AU - Wang, Jiaxuan
AU - Li, Xiaoduo
AU - Han, Liang
AU - Yu, Haoyang
AU - Ren, Zhang
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2024.
PY - 2024
Y1 - 2024
N2 - Aiming at the precise hand-over issue between the gliding phase and the terminal guidance phase of hypersonic glide vehicle, two lateral guidance laws for gilding phase under hand-over angle and hand-over time constraints are proposed independent of time-to-go and range-to-go prediction. Based on the relative relationship between the vehicle and target, considering the operational requirements of multi-angle attacks, a lateral guidance law under angle constraints is designed with utilizing the sine value of an additional heading angle. Considering the operational requirements of saturated attacks and simultaneous attacks, a lateral guidance law under time constraints using the sine value of an additional azimuth error is designed. Leveraging the dynamic equations of the hypersonic glide vehicle, transforming two guidance laws into control commands for angle of attack and bank angle, achieving precise handover under multiple constraints. The simulation and the vehicles’ modeling in this paper are implemented in the lab’s simulation platform.
AB - Aiming at the precise hand-over issue between the gliding phase and the terminal guidance phase of hypersonic glide vehicle, two lateral guidance laws for gilding phase under hand-over angle and hand-over time constraints are proposed independent of time-to-go and range-to-go prediction. Based on the relative relationship between the vehicle and target, considering the operational requirements of multi-angle attacks, a lateral guidance law under angle constraints is designed with utilizing the sine value of an additional heading angle. Considering the operational requirements of saturated attacks and simultaneous attacks, a lateral guidance law under time constraints using the sine value of an additional azimuth error is designed. Leveraging the dynamic equations of the hypersonic glide vehicle, transforming two guidance laws into control commands for angle of attack and bank angle, achieving precise handover under multiple constraints. The simulation and the vehicles’ modeling in this paper are implemented in the lab’s simulation platform.
KW - Hypersonic glide vehicle
KW - additional angular error approach
KW - lateral guidance law
UR - https://www.scopus.com/pages/publications/85200573790
U2 - 10.1007/978-981-97-3340-8_50
DO - 10.1007/978-981-97-3340-8_50
M3 - 会议稿件
AN - SCOPUS:85200573790
SN - 9789819733392
T3 - Lecture Notes in Electrical Engineering
SP - 567
EP - 579
BT - Proceedings of 2023 7th Chinese Conference on Swarm Intelligence and Cooperative Control - Swarm Guidance Technologies
A2 - Jiang, Guo-Ping
A2 - Wang, Mengyi
A2 - Ren, Zhang
PB - Springer Science and Business Media Deutschland GmbH
T2 - 7th Chinese Conference on Swarm Intelligence and Cooperative Control, CCSICC 2023
Y2 - 24 November 2023 through 27 November 2023
ER -