Earticle

초록

영어

A new kind of adaptive backstepping method is proposed for simplified missile model of pitch channel with time-varying and uncertain parameters. Backstepping control is an effective method for coping with system uncertainties. Adaptive method is integrated with backstepping method and a Lyapunov function is constructed to guarantee the whole system is stable. Through the theoretical analysis and numerical simulation, comparison between PID control and backstepping control shows that the backstepping control for the uncertain missile system has a better control effect. And compared with the PID control method, backstepping control has better robustness.

목차

Abstract
 1. Introduction
 2. Problem Description
 3. PID Control Law Design
 4. Backstepping Law Design
 5. Numerical Simulation
  5.1 Simulation of PID Control
  5.2 Simulation of Backstepping Control
  5.3 Comparison and Analysis
 6. Conclusion
 References

키워드

저자

• Jinyong Yu [ Department of control engineering, Naval aeronautical and Astronautical University, Yantai, China ]
• Junwei Lei [ Department of control engineering, Naval aeronautical and Astronautical University, Yantai, China ]
• Guoqiang Liang [ Department of control engineering, Naval aeronautical and Astronautical University, Yantai, China ]
• Di Liu [ Department of control engineering, Naval aeronautical and Astronautical University, Yantai, China ]
• Zexue Li [ Department of control engineering, Naval aeronautical and Astronautical University, Yantai, China ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Control and Automation

• 간기

  월간

• pISSN

  2005-4297

• 수록기간

  2008~2016

• 십진분류

  KDC 505 DDC 605