Adaptive parameter estimation control of nonminimum phase hypersonic flight vehicle

被引：0
作者：
Wang X. [1 ]
Xu B. [1 ]
Hong R. [2 ]
机构：
[1] School of Automation, Northwestern Polytechnical University, Xi'an
[2] Chengdu Aircraft Design and Research Institute, Chengdu
来源：
Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica | 2021年 / 51卷 / 09期
关键词：
Backstepping control; Hypersonic flight vehicle; Nonminimum phase; Output redefinition; Parameter estimation;
D O I：
10.1360/SST-2020-0211
中图分类号：
学科分类号：
摘要：
In this study, considering the longitudinal dynamic model of a nonminimum phase hypersonic flight vehicle, output-redefinition-based adaptive parameter estimation control is proposed. Output redefinition is employed to transform unstable internal dynamics to asymptotically stable internal dynamics. Based on the coordinate transformation of the redefined internal dynamics, the pitch angle command is derived and used as the reference command of the input-output subsystem. For the redefined attitude subsystem and the velocity subsystem, the unknown aerodynamic functions are decomposed into the known state vector and the unknown aerodynamic parameter vector, that is the linear parametric form. The adaptive updating laws are constructed to estimate the aerodynamic parameter vectors, and then the dynamic inversion control is designed for the velocity subsystem and the backstepping control is designed for the input-output subsystem. The system stability is analyzed via the Lyapunov stability theorem while simulation studies are conducted to illustrate the effectiveness of the proposed method. © 2021, Science Press. All right reserved.
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页码：1066 / 1074
页数：8
相关论文
共 22 条
  • [1] Xu B, Shi Z K, An overview on flight dynamics and control approaches for hypersonic vehicles, Sci China Inf Sci, 58, pp. 1-19, (2015)
  • [2] Banerjee S, Wang Z, Baur B, Et al., L1 adaptive control augmentation for the longitudinal dynamics of a hypersonic glider, J Guid Control Dyn, 39, pp. 275-291, (2016)
  • [3] Yi Y, Xu L, Shen H, Et al., Disturbance observer-based L1 robust tracking control for hypersonic vehicles with T-S disturbance modeling, Int J Adv Robotic Syst, 13, pp. 1-10, (2016)
  • [4] Xu H, Mirmirani M D, Ioannou P A, Adaptive sliding mode control design for a hypersonic flight vehicle, J Guid Control Dyn, 27, pp. 829-838, (2004)
  • [5] Xu B, Yang D, Shi Z, Et al., Online recorded data-based composite neural control of strict-feedback systems with application to hypersonic flight dynamics, IEEE Trans Neural Netw Learning Syst, 29, pp. 3839-3849, (2018)
  • [6] Gao D, Sun Z, Luo X, Et al., Fuzzy adaptive control for hypersonic vehicle via Backstepping method, Control Theory A, 5, pp. 3-8, (2008)
  • [7] Xu B, Shi Z, Sun F, Et al., Barrier lyapunov function based learning control of hypersonic flight vehicle with AOA constraint and actuator faults, IEEE Trans Cybern, 49, pp. 1047-1057, (2019)
  • [8] Zong Q, Wang F, Tian B, Et al., Robust adaptive dynamic surface control design for a flexible air-breathing hypersonic vehicle with input constraints and uncertainty, Nonlinear Dyn, 78, pp. 289-315, (2014)
  • [9] Xu B, Sun F, Pan Y, Et al., Disturbance observer based composite learning fuzzy control of nonlinear systems with unknown dead zone, IEEE Trans Syst Man Cybern Syst, 47, pp. 1854-1862, (2017)
  • [10] Parker J T, Serrani A, Yurkovich S, Et al., Control-oriented modeling of an air-breathing hypersonic vehicle, J Guid Control Dyn, 30, pp. 856-869, (2007)
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