Design of automatic control system for longitudinal landing on carrier

被引：0

作者：

Huang, De-Gang ^{[1
]}

Zhang, Wei-Guo ^{[1
]}

Shao, Shan ^{[2
]}

Wang, Zhi-Gang ^{[2
]}

Zhang, Xiu-Lin ^{[2
]}

机构：

[1] School of Automation, Northwestern Polytechnical University, Xi'an, 710129, Shaanxi

[2] Shenyang Aircraft Design Institute, Shenyang, 110035, Liaoning

来源：

Kongzhi Lilun Yu Yingyong/Control Theory and Applications | 2014年 / 31卷 / 12期

关键词：

Carrier aircraft; Command filter; Flight control system; Integral backstepping; Sliding mode control; Tuning function;

D O I：

10.7641/CTA.2014.40682

中图分类号：

学科分类号：

摘要：

When a aircraft carrier sails in the sea at a certain speed for uniform linear motion, the sea wave motivates the ship to motion in 3 degree of freedom and accompanying the interference of low altitude atmosphere turbulent flow and airwake at the same time, which makes the landing environment of carrier aircraft fair adverse. That proposes a huge challenge for the control system of autolanding. For the special problem, a method of the Command Filter Integral backstepping and Sliding Mode Control is presented in this paper. First, the command filter to deal with the problem of calculation expansion in backstepping method is adopted in this method, and then introduces of sliding mode control to handle the problems of matched uncertainty and external disturbance. In order to depress the shake of sliding mode control, using the idea of higher order sliding mode control in this paper, introducing an additional virtual control equation of state to make the outputs of control system work on the integration device, which could not only depress the chattering, but also dispose the matched and unmatched uncertainty. At last, the global stability of the proposed method is proved on the whole and the effectiveness is tested by the simulations. ©, 2014, South China University of Technology. All right reserved.

引用

页码：1731 / 1739

页数：8

共 19 条

[11]

Wang J., Hu J., Robust tracking control for a class of nonlinear systems with unmatched uncertainties, Control and Decision, 26, 5, (2011)

[12]

Li H., Dou L., Su Z., Adaptive Backstepping nonsingular fast terminal sliding mode control for mismatched uncertain systems, Control and Decision, 27, 10, (2012)

[13]

Torsten L., Integral Backstepping control of an unmanned, unstable, fin-less airship, AIAA Guidance, Navigation Control Conference, pp. 2-5, (1992)

[14]

Yu J., Feng Y., Zheng J., Suppression of mechanical resonance based on higher-order sliding mode and acceleration feedback, Control Theory & Applications, 26, 10, pp. 1133-1136, (2009)

[15]

Levant A., Higher-order sliding modes, differentiation and outputfeedback control, International Journal of Control, 76, 9-10, pp. 924-941, (2003)

[16]

Farrell J.A., Polycarpou M., Sharma M., Et al., Command filtered backstepping, IEEE Transactions on Automatic Control, 54, 6, pp. 1391-1395, (2009)

[17]

Dong W.J., Farrell J.A., Polycarpou M.M., Et al., Command filtered adaptive backstepping, IEEE Transactions on Control Systems Technology, 20, 3, pp. 566-580, (2012)

[18]

Khalil H., Nonlinear Systems, (2002)

[19]

Chen H., Zhang W., Wang X., Design of automatic control system for longitudinal landing on carrier, Journal of Missiles and Guidance, 27, 1, pp. 73-76, (2007)

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