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2000
Volume 13, Issue 3
  • ISSN: 2352-0965
  • E-ISSN: 2352-0973

Abstract

Background: This paper is devoted to adaptive feedback linearization based stabilization of a two-axis gimbal platform. Methods: A Lyapunov based adaptation mechanism is proposed for stabilization of a two axes gimbal system through a feedback linearized control structure. The uncertainty of the products of inertia is incorporated in the design procedure. Results: The performed computer simulations demonstrate the robust performance of the proposed two-axis gimbal stabilizer considering the cross-coupling effects between inner and outer gimbals. Conclusion: The proposed control structure could be utilized in guided missiles, spacecraft, and navigation systems.

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/content/journals/raeeng/10.2174/2352096512666181128095433
2020-05-01
2025-06-22
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/content/journals/raeeng/10.2174/2352096512666181128095433
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