Earticle

초록

영어

For controlling the deployment of subsatellite, the dumbbell model of tethered satellite system (TSS) is built. The paper develops a nonlinear receding horizon feedback control rule based on the nonlinear dynamics model using an indirect Legendre psuedospectral method. The nonlinear control problem is approximated with successive linear problems obtained via a quasilinearisation around reference trajectory. The feedback gains of receding horizon control could be obtained via solving a two-point boundary value problem which may be discretized into a set of linear algebraic equations by the indirect Legendre pseudospectral method. A numerical example is included to demonstrate the strong stability and high accuracy of the feedback controller under initial perturbations.

목차

Abstract
 1. Introduction
 2. Mathematical Model
 3. Nonlinear Receding Horizon Control
  3.1. Problem Formulation
  3.2. Indirect LGL Pseudospectral Discretization
  3.3. Feedback Control Gain:
 4. Numerical Example
 5. Conclusions
 Acknowledgements
 References

키워드

저자

• Guoyong Li [ School of Mechanical Engineering, Shandong University, Jinan, P.R. China, 250061, National Network Software Testing Center (Jinan) ]
• Changhou Lu [ School of Mechanical Engineering, Shandong University, Jinan, P.R. China, 250061, Key Laboratory of High-efficiency and Clean Mechanical Manufacture (Shandong University), Ministry of Education, P. R. China ] Corresponding author
• Wei Pan [ School of Mechanical Engineering, Shandong University, Jinan, P.R. China, 250061, Key Laboratory of High-efficiency and Clean Mechanical Manufacture (Shandong University), Ministry of Education, P. R. China ]
• Qing wang [ School of Mechanical Engineering, Shandong University, Jinan, P.R. China, 250061 ]

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