Modeling and Controller Design for the Air-to-Air Missile Uncertain System

Authors

  • Yanjun Liang School of Computer and Information Engineering, Anyang Normal University, Anyang 455000, China
  • Junqi Liang General Teaching Office, Shanghai Sunking Construction Management &Consulting Co. ltd., Shanghai 200070, China
  • Zhongsheng Wang Department of Automation, Guangdong Polytechnic Normal University, Guangzhou 510000, China

Keywords:

uncertain system, dynamic model, controller design, air-to-air missile system.

Abstract

The guidance and control problem of the air-to-air missile system is studied. A nonlinear, coupling dynamic model of the air-to-air missile with six degrees of freedom is investigated, and a uncertain control system is proposed according to some assumptions and simplifications. Then, based on Lyapunov stability theory, a Lyapunov function is employed, and a controller is designed for the air-to-air missile. Numerical simulations show that the control system proves the correctness and has preferably tracking performance and illustrate the effectiveness of the proposed controller.

References

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Published

2017-09-08

How to Cite

Liang, Y., Liang, J., & Wang, Z. (2017). Modeling and Controller Design for the Air-to-Air Missile Uncertain System. International Journal of Computer (IJC), 27(1), 13–19. Retrieved from https://ijcjournal.org/index.php/InternationalJournalOfComputer/article/view/1050

Issue

Vol. 27 No. 1 (2017)

Section

Articles

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