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  1. コンテンツタイプ
  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. The Institute of Space and Astronautical Science report

Synthesis of Insensitive Controllers in Linear Quadratic Control Problems

https://jaxa.repo.nii.ac.jp/records/31367
https://jaxa.repo.nii.ac.jp/records/31367
2fd1153e-2de3-406b-9e15-321a3fd20829
名前 / ファイル ライセンス アクション
SA0034936.pdf SA0034936.pdf (6.5 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Synthesis of Insensitive Controllers in Linear Quadratic Control Problems
言語 en
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
著者 KAWAGUCHI, Jun'ichiro

× KAWAGUCHI, Jun'ichiro

en KAWAGUCHI, Jun'ichiro

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出版者
出版者 宇宙科学研究所
出版者(英)
出版者 Institute of Space and Astronautical Science
書誌情報 en : The Institute of Space and Astronautical Science report

巻 605, p. 1-118, 発行日 1983-09
抄録(英)
内容記述タイプ Other
内容記述 Usually, the design objectives of control systems are not only to achieve specified performances at the nominal operational points but also to guarantee admissible performances over the range of parameter variations which inevitablly exist in the actual systems. In this paper we consider the insensitive controller which guarantees the robustness explicitly in terms of parameter variations while preserving the performance in terms of cost. There have been reported many design methods as to this subject. Some investigated the techniques which augmented the system structures such as the adaptive systems or others. But here we consider the insensitive controller design that keeps its structure as usual regulators from the view point of reliability. For this purpose we evaluate the "Additive Term Design" methods in which the proper additional terms are introduced in the covariance propagation equations or the cost equations in order to assess the deterioration of the performance index (cost). Reviewing the previous works we clarify some properties of these "Additive Term Designs". And devising a few of new approaches we show that these techniques can improve the cost surfaces and the stability and the stability margins and the sensitivity with respect to the equivalent open loop systems. To show the practical applicability, these techniques are applied to three numerical examples. One is the longitudinal autopilot of aircraft and the others are the estimation problem of radar tracking and the attitude control system of a large flexible booster. These reveal that the "Additive Term Design" techniques are very effective to those systems and that particularly the M.C.V. ("Maximum Cost Variation") method improves the cost surfaces satisfactorily. Since this robustness realization requires only a slight cost increase at the nominal operational point, these techniques are expected to be applied to a large number of systems with satisfactory improvement.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0285-6808
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA10632072
資料番号
内容記述タイプ Other
内容記述 資料番号: SA0034936000
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