TY - JOUR
T1 - Fixed-Time Neural Network-Based Dynamic Surface Control for Hypersonic Flight Vehicle With Historical Data Online Learning
AU - Gao, Han
AU - Liu, Xuelin
AU - Wang, Jiale
AU - Cui, Bing
AU - Xia, Yuanqing
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2024
Y1 - 2024
N2 - The motivation of this paper is to solve the tracking control problem of hypersonic flight vehicle (HFV) with uncertainties. To this end, a fixed-time neural network (NN)-based dynamic surface control scheme is proposed. First, a historical data online learning NN is designed to handle the matched uncertainty. For the proposed NN, a fixed-time auxiliary system is utilized to introduce historical information into the update law of NN weights. This design not only improves the data utilization of the NN but also enhances the estimation performance. Then, based on the reconstructed information of NN, a fixed-time dynamic surface controller is proposed, in which a fixed-time filter is used to estimate the derivative of the virtual control input and unmatched uncertainty in HFV system. Compared with existing results, the proposed method ensures that the tracking error converges within a fixed time while having a smaller computational burden. These properties are of great importance for the practical HFV application. Finally, the effectiveness of the proposed fixed-time control strategy is verified by a numerical simulation example.
AB - The motivation of this paper is to solve the tracking control problem of hypersonic flight vehicle (HFV) with uncertainties. To this end, a fixed-time neural network (NN)-based dynamic surface control scheme is proposed. First, a historical data online learning NN is designed to handle the matched uncertainty. For the proposed NN, a fixed-time auxiliary system is utilized to introduce historical information into the update law of NN weights. This design not only improves the data utilization of the NN but also enhances the estimation performance. Then, based on the reconstructed information of NN, a fixed-time dynamic surface controller is proposed, in which a fixed-time filter is used to estimate the derivative of the virtual control input and unmatched uncertainty in HFV system. Compared with existing results, the proposed method ensures that the tracking error converges within a fixed time while having a smaller computational burden. These properties are of great importance for the practical HFV application. Finally, the effectiveness of the proposed fixed-time control strategy is verified by a numerical simulation example.
KW - Dynamic surface control
KW - fixed-time
KW - historical data online learning
KW - hypersonic flight vehicle
UR - http://www.scopus.com/inward/record.url?scp=85208669964&partnerID=8YFLogxK
U2 - 10.1109/TAES.2024.3491057
DO - 10.1109/TAES.2024.3491057
M3 - Article
AN - SCOPUS:85208669964
SN - 0018-9251
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
ER -