Earticle

초록

영어

Since the model of hypersonic missile cannot be built accurately and it can change unpredictably, traditional design method is not very effective. A synchronizing control method is introduced in this paper. A synchronizing system that has the similar structures with the controlled system is constructed, then a control law is design to make the synchronizing system trace the controlled system. So the controlled system can be controlled by controlling the synchronizing system. Finally, detailed numerical simulation was done and it showed that the synchronous control method is proved to be more effective than PID control method.

목차

Abstract
 1. Introduction
 2. Model Description
 3. Design Synchronizing Control Law
 4. Numerical Simulation
  4.1 Constant Perturbation
 5. Conclusion
 References

키워드

저자

• Aili Liu [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai Shandong 264001, China ]
• Lingling Wang [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai Shandong 264001, China ]
• Jianhong Shi [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai Shandong 264001, China ]
• Junwei Lei [ Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai Shandong 264001, China ]
• Jun Peng [ Receiving and Training Center of New Equipments, Naval Aeronautical and Astronautical University, Yantai, China ]
• Yuqiang Jin [ Department of Training, 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