自动化学报2025，Vol.51Issue(11)：2486-2497,12.DOI:10.16383/j.aas.c250279
高超声速飞行器基于Tube的鲁棒模型预测跟踪控制
Tube-based Robust Model Predictive Tracking Control for Hypersonic Flight Vehicle
摘要
Abstract
This paper addresses the tracking control problem for hypersonic flight vehicle(HFV)subject to un-known environmental disturbances and actuator faults.A composite Tube-based robust model predictive control ap-proach is proposed.Firstly,the input/output linearization of the HFV longitudinal motion model is achieved by us-ing the nonlinear dynamic inversion method,effectively decoupling the altitude and velocity control loops.Sub-sequently,robust tightened constraints are derived by incorporating Tube invariant set theory,explicitly integrat-ing both the control input magnitude and rate constraints of the HFV.Based on these constraints,a composite ro-bust model predictive control strategy is designed.Furthermore,the recursive feasibility of the proposed method is investigated,while the closed-loop stability of the control strategy is rigorously proven based on Lyapunov stability theory.Finally,simulation experiments demonstrate the effectiveness of the proposed method.关键词
高超声速飞行器/非线性动态逆/鲁棒模型预测控制/抗干扰控制Key words
Hypersonic flight vehicle/nonlinear dynamic inversion/robust model predictive control/anti-disturb-ance control引用本文复制引用
姚秀明,邢文龙,韩一睿..高超声速飞行器基于Tube的鲁棒模型预测跟踪控制[J].自动化学报,2025,51(11):2486-2497,12.基金项目
国家自然科学基金(62273029)资助Supported by National Natural Science Foundation of China(62273029) （62273029）
