Nonlinear Control for Missile Terminal Guidance-Reference-Cited by-同舟云学术

Nonlinear Control for Missile Terminal Guidance

Published:2000-02-04 Issue:4 Volume:122 Page:663-668
ISSN:0022-0434
Container-title:Journal of Dynamic Systems, Measurement, and Control
language:en
Short-container-title:

Author:

Liaw Der-Cherng¹,Liang Yew-Wen¹,Cheng Chiz-Chung¹

Affiliation:

1. Department of Electrical and Control Engineering, National Chiao Tung University, Hsinchu 30010, Taiwan, Republic of China

Abstract

Variable Structure Control (VSC) technique is applied to the design of robust homing missile guidance laws. In the design procedure, the target’s maneuver is assumed to be unpredictable and is considered as disturbances. Guidance laws are then proposed to achieve the interception performance for both cases of longitude-axis control being available and unavailable. The proposed guidance laws are continuous which alleviate chattering drawback by classic VSC design. Results are obtained and compared with those by realistic true proportional navigation design to illustrate the benefits of the proposed design. [S0022-0434(00)00604-3]

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Link

http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/122/4/663/5779118/663_1.pdf

Reference17 articles.

1. Axelband, E. Z., and Hardy, F. W., 1970, “Quasi Optimal Proportional Navigation,” IEEE Trans. Autom. Control, AC-15, No. 6, pp. 620–626.

2. Arbenz, K. , 1970, “Proportional Navigation of Nonstationary Targets,” IEEE Trans. Aerosp. Electron. Syst., AES-6, No. 4, pp. 455–457.

3. Kim, Y. S., Cho, H. S., and Bien, Z., 1985, “A New Guidance Law for Homing Missile,” J. Guid. Control Dyn., 8, No. 3, pp. 402–404.

4. Yang, C.-D., and Yeh, F. B., 1989, “General Guidance Law for Homing Missile,” IEEE Trans. Aerosp. Electron. Syst., 25, No. 2, pp. 197–211.

5. Becker, K. , 1990, “Closed-form Solution of Pure Proportional Navigation,” IEEE Trans. Aerosp. Electron. Syst., 26, No. 3, pp. 526–532.

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Robust relatively optimal trajectory tracking control for a class of uncertain nonlinear control affine systems with state and input constraints;Nonlinear Dynamics;2022-08-31

2. Observer-Based Adaptive Sliding Mode Control for Nonlinear Stochastic Markov Jump Systems via T–S Fuzzy Modeling: Applications to Robot Arm Model;IEEE Transactions on Industrial Electronics;2021-01

3. Vibration Reduction of the Nonlinearly Tufted Carpet Yarn by a Modified Sliding Mode Control Method;Shock and Vibration;2019-04-28

4. On an Optimized Fuzzy Supervized Multiphase Guidance Law;Asian Journal of Control;2016-02-02

5. Finite Time Convergence Guidance Law Accounting for Missile Autopilot;Journal of Dynamic Systems, Measurement, and Control;2015-05-01