書誌事項
- タイトル別名
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- On the Characteristic Equation and Stabilizing Conditions of Flexible Structure Control Systems
- ジュウナン コウゾウブツ セイギョケイ ノ トクセイ ホウテイシキ ト アンテ
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Precise attitude and shape control of flexible spacecraft requires active control of flexural vibrations. This paper first derives a general closed loop characteristic equation of a flexural vibration control system equipped with arbitrary numbers of non-point actuators and sensors whose regions of actions and observations are expressed by weight functions. Then, the characteristic equation in a determinantal form is expanded in a mathematically tractable form in which each coefficient is a product of an actuator-dependent determinant, a sensor-dependent determinant and a compensator-dependent determinant. By applying the perturbation technique to the expanded characteristic equation, it is shown that a modal stabilizing condition can be obtained for a rate and position feedback control system. Finally, a numerical example is given to illustrate the usage of the condition.
収録刊行物
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- システム制御情報学会論文誌
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システム制御情報学会論文誌 2 (10), 343-349, 1989
一般社団法人 システム制御情報学会
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詳細情報 詳細情報について
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- CRID
- 1390282680143556480
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- NII論文ID
- 130002038568
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- NII書誌ID
- AN1013280X
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- ISSN
- 2185811X
- 13425668
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- NDL書誌ID
- 3256678
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- データソース種別
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- JaLC
- NDL
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- 抄録ライセンスフラグ
- 使用不可