Reinforcement Learning–Based Adaptive Attitude Control Method for a Class of Hypersonic Flight Vehicles Subject to Nonaffine Structure and Unmatched DisturbancesSource: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 002::page 04024003-1DOI: 10.1061/JAEEEZ.ASENG-5008Publisher: ASCE
Abstract: This paper proposes a reinforcement learning–based adaptive attitude control (RLAC) method for a class of hypersonic flight vehicles (HFVs) output constrained nonaffine attitude control problems subject to unmatched disturbances. First, by considering the strong coupling of HFVs attitude dynamics, the uncertainty of aerodynamic parameters and the complexity of the flight environment, a second-order multivariable nonaffine nonlinear control system is obtained. Then, by introducing specific nonlinear function and coordinate transformation techniques, the output constrained nonaffine control problem is transformed into a stabilization problem of several new variables. Moreover, dual actor-critic networks and their adaptive weight update laws are designed to cope with unknown unmatched and matched structural uncertainties. Meanwhile, two super-twisting disturbance observers integrated with dual actor-critic networks are designed to compensate unknown unmatched and matched external disturbances. With the help of the Lyapunov direct method, output constraint, convergence of the estimated weights, and stability of the system are proved. Finally, the validity as well as superiority of the proposed method are verified by numerical simulations.
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contributor author | Zheng Wang | |
contributor author | Tianyi Wu | |
contributor author | Zhanxia Zhu | |
contributor author | Chunhe Ma | |
date accessioned | 2024-04-27T22:39:13Z | |
date available | 2024-04-27T22:39:13Z | |
date issued | 2024/03/01 | |
identifier other | 10.1061-JAEEEZ.ASENG-5008.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4297174 | |
description abstract | This paper proposes a reinforcement learning–based adaptive attitude control (RLAC) method for a class of hypersonic flight vehicles (HFVs) output constrained nonaffine attitude control problems subject to unmatched disturbances. First, by considering the strong coupling of HFVs attitude dynamics, the uncertainty of aerodynamic parameters and the complexity of the flight environment, a second-order multivariable nonaffine nonlinear control system is obtained. Then, by introducing specific nonlinear function and coordinate transformation techniques, the output constrained nonaffine control problem is transformed into a stabilization problem of several new variables. Moreover, dual actor-critic networks and their adaptive weight update laws are designed to cope with unknown unmatched and matched structural uncertainties. Meanwhile, two super-twisting disturbance observers integrated with dual actor-critic networks are designed to compensate unknown unmatched and matched external disturbances. With the help of the Lyapunov direct method, output constraint, convergence of the estimated weights, and stability of the system are proved. Finally, the validity as well as superiority of the proposed method are verified by numerical simulations. | |
publisher | ASCE | |
title | Reinforcement Learning–Based Adaptive Attitude Control Method for a Class of Hypersonic Flight Vehicles Subject to Nonaffine Structure and Unmatched Disturbances | |
type | Journal Article | |
journal volume | 37 | |
journal issue | 2 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/JAEEEZ.ASENG-5008 | |
journal fristpage | 04024003-1 | |
journal lastpage | 04024003-12 | |
page | 12 | |
tree | Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 002 | |
contenttype | Fulltext |