REORIENTATION MANEUVER OF A SPACECRAFT COMPOSED OF TWO RIGID BODIES

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概要

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• In this paper, attitude control of a spacecraft which consists of two rigid bodies coupled by a ball joint is discussed. First, we propose a time-invariant discontinuous feedback controller for a class of nonholonomic systems, first order systems, based on Lyapunov control. The first order system is a system where the input vector fields and the first level of Lie brackets between them span the tangent space at each configuration. Next, the controller is applied to the spacecraft when the angular momentum of the system is zero, and the effectiveness of the controller is verified by numerical simulations.

• 一般社団法人日本機械学会の論文

著者

• Tada Yukio

  Dept. Of Human & Mechanical Systems Engineering Kanazawa University

• Tada Yukio

  Dept. Of Computer And Systems Engineering Faculty Of Engineering Kobe University

• Urakubo Takateru

  Dept. of Computer and Systems Engineering, Faculty of Engineering, Kobe University

• Tsuchiya Kazuo

  Dept. of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University

• Urakubo Takateru

  Dept. Of Computer And Systems Engineering Faculty Of Engineering Kobe University

• Tsuchiya Kazuo

  Dept. Of Aeronautics And Astronautics Graduate School Of Engineering Kyoto University

関連論文

• REORIENTATION MANEUVER OF A SPACECRAFT COMPOSED OF TWO RIGID BODIES
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