TY - JOUR
T1 - Data-Based Suboptimal Tracking Control for Hypersonic Flight Vehicle Subject to Input Delay, Input Amplitude Constraint, and Input Rate Constraint
AU - Hu, Xiaoxiang
AU - Dong, Kejun
AU - Xu, Jingwen
AU - Xiao, Bing
N1 - Publisher Copyright:
© 2025 John Wiley & Sons Ltd.
PY - 2025
Y1 - 2025
N2 - A suboptimal tracking controller is designed for hypersonic flight vehicle (HFV) subject to input delay, input amplitude constraint, and input rate constraint in this article. The input delay, input amplitude constraint, and input rate constraint are all caused by physical constraints of HFV, and are inevitable, so they must be considered in controller design. The model of input delay, input amplitude constraint and input rate constraint are first developed and then they are all transformed into inequality constraints. With considered the inequality constraints, precompensation method is utilized and then the tracking controller design problem for HFV with inequality constraints is transformed into controller design of unconstrained augmented system. The optimal controller for the unconstrained augmented system can be viewed as suboptimal controller for HFV. Then with considered the advantage of reinforcement learning (RL), an online policy-iteration (PI) algorithm for the optimal controller of the unconstrained augmented system is given. Furthermore, considering the uncertainty and unmodeled dynamics of HFV, neural networks (NN) are utilized and a data-based solution strategy of integral reinforcement learning (IRL) is presented for the unconstrained augmented system. Simulation results on the nonlinear model of HFV are given to reflect the effectiveness of the designed method.
AB - A suboptimal tracking controller is designed for hypersonic flight vehicle (HFV) subject to input delay, input amplitude constraint, and input rate constraint in this article. The input delay, input amplitude constraint, and input rate constraint are all caused by physical constraints of HFV, and are inevitable, so they must be considered in controller design. The model of input delay, input amplitude constraint and input rate constraint are first developed and then they are all transformed into inequality constraints. With considered the inequality constraints, precompensation method is utilized and then the tracking controller design problem for HFV with inequality constraints is transformed into controller design of unconstrained augmented system. The optimal controller for the unconstrained augmented system can be viewed as suboptimal controller for HFV. Then with considered the advantage of reinforcement learning (RL), an online policy-iteration (PI) algorithm for the optimal controller of the unconstrained augmented system is given. Furthermore, considering the uncertainty and unmodeled dynamics of HFV, neural networks (NN) are utilized and a data-based solution strategy of integral reinforcement learning (IRL) is presented for the unconstrained augmented system. Simulation results on the nonlinear model of HFV are given to reflect the effectiveness of the designed method.
KW - data-based control
KW - hypersonic flight vehicle (HFV)
KW - input amplitude constraint
KW - input delay
KW - input rate constraint
KW - integral reinforcement learning
UR - http://www.scopus.com/inward/record.url?scp=105006903143&partnerID=8YFLogxK
U2 - 10.1002/rnc.8052
DO - 10.1002/rnc.8052
M3 - 文章
AN - SCOPUS:105006903143
SN - 1049-8923
JO - International Journal of Robust and Nonlinear Control
JF - International Journal of Robust and Nonlinear Control
ER -