Earticle

초록

영어

This paper designs the feedback controller for the unstable Dutch Roll and severe kinematic coupling of the hypersonic vehicle at high angle of attack and large mach number. This paper deduces the mechanism of improving the stability of the Dutch Roll and illustrates the mechanism of restraining the kinematic coupling using controller based on the linear small perturbation equations. And an easy analysis is made about the signal of controller. Finally, the relational tests are conducted in simulations using controller. The simulation result shows that the controller can improve the damp of the Dutch Roll, weaken the influence of kinematic coupling, restrain the variety of sideslip and improve the equality of sideslip.

목차

Abstract
 1. Introduction
 2. Mathematical Model
 3. The Mechanism of b Feedback Control
  3.1. b feedback Stability Augmentation the Dutch Roll
  3.2. b Feedback Eliminates the Kinematic Coupling
  3.3. b Signal Analysis
 4. Simulation
 5. Conclusion
 References

키워드

저자

• Liang-liang Yin [ College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China ]
• Yi-min Huang [ College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China ]
• Chun-zhen Sun [ College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China ]
• Jie Jia [ College of Information Engineering, Nanchang Hangkong University, Nanchang, China ]
• Yong Yang [ School of Information Technology, Jiangxi University of Finance and Economics, Nanchang, 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