State-reconstruction-based robust backstepping control of air-breathing hypersonic vehicles

被引：5

作者：

Bu, Xiang-Wei ^{[1
]}

Wu, Xiao-Yan ^{[1
]}

Ma, Zhen ^{[1
]}

Zhang, Rui ^{[1
]}

机构：

[1] Air and Missile Defense College, Air Force Engineering University, Xi'an

来源：

Guti Huojian Jishu/Journal of Solid Rocket Technology | 2015年 / 38卷 / 03期

关键词：

Air-breathing hypersonic vehicles; Arctangent tracking differentiator; Nonlinear disturbance observer; Nonlinear-linear tracking differentiator; Robust backstepping controller; State reconstruction;

D O I：

10.7673/j.issn.1006-2793.2015.03.003

中图分类号：

学科分类号：

摘要：

A robust backstepping controller was designed based on state reconstruction for flexible air-breathing hypersonic vehicles considering that only the velocity, altitude and pitch rate were observable. Firstly, the controlled plant was rewritten as a strict feedback form, and the actual control laws and virtual control laws were designed based on dynamic inversion and backstepping respectively. Secondly, arctangent tracking differentiator was introduced to estimate the derivatives of virtual control laws and reconstruct the states of flight-path angle and angle of attack. Finally, in order to guarantee the backstepping controller' robustness, a new nonlinear disturbance observer was designed based on nonlinear-linear tracking differentiator to estimate and compensate uncertainties of the model precisely. Simulation results show that a high precise state construction can be obtained by the proposed strategy and the presented control methodology can provide a stable altitude and velocity tracking, and eliminate the influence of the uncertainties of the model. ©, 2015, Journal of Solid Rocket Technology. All right reserved.

引用

页码：314 / 319and355

共 7 条

[1]

Fiorentini L., Serrani A., Adaptive restricted trajectory tracking for a non-minimum phase hypersonic vehicle model, Automatica, 48, pp. 1248-1261, (2012)

[2]

Zong Q., Wang J., Tian B.-L., Et al., Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle, Aerospace Science and Technology, 27, pp. 127-137, (2013)

[3]

Sigthorsson D.O., Jankovsky P., Serrani A., Et al., Robust linear output feedback control of an airbreathing hypersonic vehicle, Journal of Guidance, Control, and Dynamics, 31, 4, pp. 1052-1066, (2008)

[4]

Zhang Z., Hu J., Stability analysis of a hypersonic vehicle controlled by the characteristic model based adaptive controller, Science China (Information Sciences), 55, pp. 2243-2256, (2012)

[5]

Xu H.-J., Mirmirani M.D., Ioannou P.A., Adaptive sliding mode control design for a hypersonic flight vehicle, Journal of Guidance, Control, and Dynamics, 27, 5, pp. 829-838, (2004)

[6]

Yang J., Li S.-H., Sun C.-Y., Nonlinear-disturbance-observer-based robust flight control for airbreathing hypersonic vehicles, IEEE Transactions on Aerospace and Electronic Systems, 49, 2, pp. 1263-1275, (2013)

[7]

Fiorentini L., Nonlinear adaptive controller design for air-breathing hypersonic vehicles, (2010)

← 1 →