書誌事項
- タイトル別名
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- Computational Method of Optimal Control Problem Using Mathematical Programming. (1st Report). Introduction of Sensitivity Differential Equations.
- スウリ ケイカクホウ オ モチイタ サイテキ セイギョ モンダイ カイホウ ニ
- Introduction of Sensitivity Differential Equations
- 感度微分方程式の導入
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抄録
This paper considers a numerical method for optimal control problems which are solved by using a mathematical programming formulation. The sensitivity differential equations are obtained to calculate the derivative information of the objective and constraint functions. Numerical examples of the accent trajectory problem of a spaceplane compare the proposed method with the conventional method which calculates derivatives using finite difference approximation. The results demonstrate the improvement of accuracy and computational efficiency of the present method.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 45 (519), 231-237, 1997
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679454254592
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- NII論文ID
- 10002861497
- 10004209252
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
- http://id.crossref.org/issn/13446460
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- NDL書誌ID
- 4184050
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可