Robust control system for Spacecraft Motion Trajectory

Authors

  • Samigulina Ildusovna Zarina doctorat PhD
  • Shiryeva Ivanovna Olga candidate of technical science, docent
  • Samigulina Ahmetovna Galina doctor of technical science, docent
  • Fourati Ben Mahmoud Hassen associate professor

Keywords:

Robust control system, Spacecraft Motion Trajectory, adaptive control approach, nonlinear system modeling, reference model, Lyapunov method.

Abstract

In aerospace field the economic realization of a spacecraft is one of the main objectives which should be accomplished by conceiving the optimal propulsion system and best control programs. This article focuses on the implementation of uncertain control system theory and development of a robust control system of Spacecraft Motion Trajectory (SMT). The proposed strategy involves the nonlinear mathematical model of SMT expressed in the central field, which is linearized by the Taylor expansion, and model reference Adaptive Control Approach (ACA) with the second Lyapunov method to offer a high rate and unfailing performance in the functioning. The efficiencies of the linearization procedure and the control approach are theoretically investigated through some realistic simulations and tests under Matlab.

Author Biographies

  • Samigulina Ildusovna Zarina, doctorat PhD
    Lecturer of departament 
    "Automation and control",
    Institute of Information and Telecommunication Technologies, KazNTU named K.I.Satpayev.
  • Shiryeva Ivanovna Olga, candidate of technical science, docent
    Senior Reseacher of the Laboratory «Intellectual control systems and networks», Institute of Informatics and control Problems. 
  • Samigulina Ahmetovna Galina, doctor of technical science, docent
    Chief of the Laboratory «Intellectual control systems and networks», Institute of Informatics and control Problems. 
  • Fourati Ben Mahmoud Hassen, associate professor
    Senoir Reseacher of the Networked Controlled System Team (NeCS), GIPSA-LAB, Automation and Control Department, University Joseph Fourier

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Published

2014-08-01

Issue

Vol. 7 No. 3: (July 2014)

Section

Industrial and Managerial Mathematics

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How to Cite

Robust control system for Spacecraft Motion Trajectory. (2014). European Journal of Pure and Applied Mathematics, 7(3), 289-303. https://www.ejpam.com/index.php/ejpam/article/view/2135