Nonlinear Optimal Feedback Control for Deployment/Retrieval of a Tethered Satellite

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概要

• 論文の詳細を見る

• Nonlinear optimal state feedback control is designed for the deployment and retrieval of a tethered satellite in the orbital plane. The mass and flexibility of the tether are neglected, and the controlled system is expressed by a bilinear state equation. To stabilize the system asymptotically, the receding horizon control is applied with the terminal state constrained to be zero. As a practical approach to the problem, the time-dependent penalty function method is employed to achieve the terminal constraint asymptotically, and an algorithm is derived so that an increase of the terminal penalty will cause no numerical difficulty. The effectiveness and robustness of the present approach are confirmed in numerical simulations.

• 社団法人 日本航空宇宙学会の論文
• 2001-02-04

著者

• OHTSUKA Toshiyuki

  Department of Environmental Sciences, Faculty of Science, Ibaraki University

• Ohtsuka Toshiyuki

  Department Of Computer-controlled Mechanical System Osaka University

関連論文

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• Nonlinear Optimal Feedback Control for Deployment/Retrieval of a Tethered Satellite
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• l_1 State Feedback Control of Active Suspension
• Nonlinear Receding-Horizon State Estimation with Unknown Disturbances
• Receding Horizon Control for High-Dimensional Burgers' Equations with Boundary Control Inputs

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