Earticle

초록

영어

The backstepping design method has been used to design the control system of the Bank-to-turn (BTT) missile, which depends on the designer’s personal experience and a large number of complicated iterative calculation, and needs to consume a lot of time throughout the design process. To solve this problem, a missile control system surrogate model is established by using Kriging meta-model. After establishing the surrogate model, the genetic algorithm is applied to the control system optimal solution. The proposed method can obtain a set of control parameters that minimizes the performance function by searching the given control parameters space. The simulation results show that the method can reduce the amount of calculations and achieve the desired control parameters effectively.

목차

Abstract
 1. Introduction
 2. Missile Control System Design
  2.1. BTT Missile Modeling
  2.2. Structure of Missile Control System
  2.3. The Backstepping Controller Design
 3. The Missile Control System Optimization
  3.1. Construct the Kriging Approximation Model
  3.2. Optimal Algorithm
 4. The Results of Simulation and Analysis
 5. Conclusion
 Acknowledgements
 References

키워드

저자

• Jiakun Zheng [ College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan province, 410073 ]
• Ying Liao [ College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan province, 410073 ]
• Yajun Yang [ College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan province, 410073 ]

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