TY - JOUR
T1 - Robust Tracking for Hypersonic Reentry Vehicles via Disturbance Estimation-Triggered Control
AU - Guo, Zongyi
AU - Guo, Jianguo
AU - Zhou, Jun
AU - Chang, Jing
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2020/4
Y1 - 2020/4
N2 - This note presents a novel control framework based on disturbance estimation information to exploit the potential performance improvement. Disturbances in the hypersonic reentry vehicles are revisited, and a disturbance effect indicator (DEI) is defined to demonstrate the pros and cons of disturbances' influence on the system. Based on the disturbance estimation, a disturbance estimation-triggered control scheme for the attitude tracking is established. Furthermore, the ultimately bounded stability of the closed-loop system is guaranteed. Distinguished from eliminating the disturbance directly in the state-of-the-art disturbance observer-based control, the proposed control switches its structure to counteract or retain the disturbance according to the DEI, and thus is capable of improving the transient performance. Simulation results verify the effectiveness and superiority of the proposed approach.
AB - This note presents a novel control framework based on disturbance estimation information to exploit the potential performance improvement. Disturbances in the hypersonic reentry vehicles are revisited, and a disturbance effect indicator (DEI) is defined to demonstrate the pros and cons of disturbances' influence on the system. Based on the disturbance estimation, a disturbance estimation-triggered control scheme for the attitude tracking is established. Furthermore, the ultimately bounded stability of the closed-loop system is guaranteed. Distinguished from eliminating the disturbance directly in the state-of-the-art disturbance observer-based control, the proposed control switches its structure to counteract or retain the disturbance according to the DEI, and thus is capable of improving the transient performance. Simulation results verify the effectiveness and superiority of the proposed approach.
KW - Disturbance effect indicator
KW - disturbance estimation-triggered control
KW - disturbance observer
KW - hypersonic reentry vehicles
UR - http://www.scopus.com/inward/record.url?scp=85083435707&partnerID=8YFLogxK
U2 - 10.1109/TAES.2019.2928605
DO - 10.1109/TAES.2019.2928605
M3 - 文章
AN - SCOPUS:85083435707
SN - 0018-9251
VL - 56
SP - 1279
EP - 1289
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 2
M1 - 8762156
ER -