Earticle

초록

영어

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

목차

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

키워드

저자

• Jinyong Yu [ Department of Control Engineering, Naval Aeronautical and Astronautical University, China ]
• Junwei Lei [ Department of Control Engineering, Naval Aeronautical and Astronautical University, China ]
• Di Liu [ Department of Control Engineering, Naval Aeronautical and Astronautical University, China ]
• Zexue Li [ Department of Control Engineering, Naval Aeronautical and Astronautical University, China ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Hybrid Information Technology

• 간기

  격월간

• pISSN

  1738-9968

• 수록기간

  2008~2016

• 십진분류

  KDC 505 DDC 605