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Optimization Issues in the Problem of Small Satellite Attitude Determination and Control

In: Modeling and Optimization in Space Engineering

Author

Listed:
  • Zaure Rakisheva

    (Al-Farabi Kazakh National University)

  • Anna Sukhenko

    (Al-Farabi Kazakh National University)

  • Nazgul Kaliyeva

    (Al-Farabi Kazakh National University)

Abstract

The problems of synthesis of attitude determination and control system of small satellites regarding the influence of external perturbations due to their small mass and restrictions in using high-precision actuators, due to the limitations of energy budget and construction, are considered. The solutions to this problem are proposed involving the development of high-accuracy algorithms for satellite attitude determination and control, using the minimum set of sensors, various types of actuators, and optimization principles.

Suggested Citation

  • Zaure Rakisheva & Anna Sukhenko & Nazgul Kaliyeva, 2019. "Optimization Issues in the Problem of Small Satellite Attitude Determination and Control," Springer Optimization and Its Applications, in: Giorgio Fasano & János D. Pintér (ed.), Modeling and Optimization in Space Engineering, pages 373-393, Springer.
    • Handle: RePEc:spr:spochp:978-3-030-10501-3_14
    DOI: 10.1007/978-3-030-10501-3_14
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