TY - JOUR
T1 - Novel Explicit Reference Governor-Based Adaptive Terminal Sliding Mode Control Design for Reentry Vehicles Equipped with Strapdown Seeker
AU - Guo, Jianguo
AU - Lu, Ningbo
AU - Jiang, Ruimin
AU - Guo, Zongyi
N1 - Publisher Copyright:
© 2023, The Author(s), under exclusive licence to The Korean Society for Aeronautical & Space Sciences.
PY - 2024/1
Y1 - 2024/1
N2 - This paper investigates an integrated guidance and control (IGC) strategy for reentry vehicles equipped with a strapdown seeker subject to the body line-of-sight (BLOS) angle constraint. A novel explicit reference governor-based IGC scheme is proposed to deal with BLOS angle constraint caused by strapdown mechanism. Taking the symmetric constraint interval as an example, the explicit reference governor is constructed for the positive and negative half intervals, respectively. The adaptive terminal sliding mode control (ATSMC) is subsequently designed for the IGC model to ensure that the closed-loop system tracks the commands of the explicit reference governor (ERG), thereby guaranteeing compliance with BLOS angle constraint. The stability of the closed-loop system is rigorously analyzed according to the Lyapunov stability theory. The numerical simulation results demonstrate the effectiveness of the proposed approach.
AB - This paper investigates an integrated guidance and control (IGC) strategy for reentry vehicles equipped with a strapdown seeker subject to the body line-of-sight (BLOS) angle constraint. A novel explicit reference governor-based IGC scheme is proposed to deal with BLOS angle constraint caused by strapdown mechanism. Taking the symmetric constraint interval as an example, the explicit reference governor is constructed for the positive and negative half intervals, respectively. The adaptive terminal sliding mode control (ATSMC) is subsequently designed for the IGC model to ensure that the closed-loop system tracks the commands of the explicit reference governor (ERG), thereby guaranteeing compliance with BLOS angle constraint. The stability of the closed-loop system is rigorously analyzed according to the Lyapunov stability theory. The numerical simulation results demonstrate the effectiveness of the proposed approach.
KW - Adaptive terminal sliding mode control
KW - Body line-of-sight angle constraint
KW - Explicit reference governor
KW - Integrated guidance and control
KW - Reentry vehicles
UR - http://www.scopus.com/inward/record.url?scp=85166923358&partnerID=8YFLogxK
U2 - 10.1007/s42405-023-00647-8
DO - 10.1007/s42405-023-00647-8
M3 - 文章
AN - SCOPUS:85166923358
SN - 2093-274X
VL - 25
SP - 200
EP - 212
JO - International Journal of Aeronautical and Space Sciences
JF - International Journal of Aeronautical and Space Sciences
IS - 1
ER -