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논문검색

The Design of Overload Synchronizing Controller Based on the Model of Supersonic Missile’s Feature Points

원문정보

Aili Liu, Lingling Wang, Jianhong Shi, Junwei Lei, Jun Peng, Yuqiang Jin

보안공학연구지원센터(IJCA) International Journal of Control and Automation Vol.9 No.2 2016.02 pp.249-260
피인용수 : 0건 (자료제공 : 네이버학술정보)

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

저자정보

  • 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

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