TY - GEN
T1 - Sliding Mode Based Line-of-Sight Tracking for Hypersonic Gliding Vehicle
AU - Han, Wanru
AU - Wang, Jie
AU - Liu, Junhui
AU - Shan, Jiayuan
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.
PY - 2025
Y1 - 2025
N2 - Aiming to design the three-dimensional trajectory tracking controller for hypersonic gliding vehicle under external disturbances, this paper presents a decoupling control strategy. The longitudinal height controller is designed based on proportional-derivative and the lateral line-of-sight (LOS) tracking controller is proposed based on terminal sliding mode. Firstly, the dynamic model of hypersonic gliding vehicles is presented. Then, the three-dimensional trajectory tracking problem is divided into longitudinal and lateral plane. Each waypoint is tracked using the height controller and the LOS tracking controller based on adaptive circle of acceptance, respectively. Finally, considering external disturbances, the LOS tracking based on sliding mode control (SMC) with power reaching law is designed and the stability of the closed-loop control system is proved. The Common Aero Vehicle (CAV) is used in numerical simulation, and the simulation results shows that under the influence of external disturbance, the trajectory tracking controller designed in this paper can track three-dimensional waypoints with high precision and stability.
AB - Aiming to design the three-dimensional trajectory tracking controller for hypersonic gliding vehicle under external disturbances, this paper presents a decoupling control strategy. The longitudinal height controller is designed based on proportional-derivative and the lateral line-of-sight (LOS) tracking controller is proposed based on terminal sliding mode. Firstly, the dynamic model of hypersonic gliding vehicles is presented. Then, the three-dimensional trajectory tracking problem is divided into longitudinal and lateral plane. Each waypoint is tracked using the height controller and the LOS tracking controller based on adaptive circle of acceptance, respectively. Finally, considering external disturbances, the LOS tracking based on sliding mode control (SMC) with power reaching law is designed and the stability of the closed-loop control system is proved. The Common Aero Vehicle (CAV) is used in numerical simulation, and the simulation results shows that under the influence of external disturbance, the trajectory tracking controller designed in this paper can track three-dimensional waypoints with high precision and stability.
KW - Hypersonic Gliding Vehicle
KW - LOS Tracking
KW - Terminal Sliding Mode Control
KW - Waypoint-Tracking Controller
UR - https://www.scopus.com/pages/publications/105000246501
U2 - 10.1007/978-981-96-2260-3_26
DO - 10.1007/978-981-96-2260-3_26
M3 - Conference contribution
AN - SCOPUS:105000246501
SN - 9789819622597
T3 - Lecture Notes in Electrical Engineering
SP - 259
EP - 270
BT - Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 16
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Deng, Yimin
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2024
Y2 - 9 August 2024 through 11 August 2024
ER -