A Study on the Numerical Method for Simultaneous Optimization of Spaceplane Design and its Flight Trajectory.

• TSUCHIYA Takeshi

  東京大学大学院工学系研究科航空宇宙工学専攻

• SUZUKI Shinji

  東京大学大学院工学系研究科航空宇宙工学専攻

Bibliographic Information

Other Title

• スペースプレーンの機体設計と飛行経路の同時最適化に関する数値解法
• スペースプレーン ノ キタイ セッケイ ト ヒコウ ケイロ ノ ドウジ サイテ

Abstract

The numerical method to solve simultaneous design and control optimization problems is considered. Firstly, the simultaneous optimization problem dealt with in this paper is defined, and this problem is transformed into a new formulated nonlinear programming problem. Considering that the nonlinear programming problem is solved by using a sequential quadratic programming method, the diagonal form of the Hessian matrix for the Lagrange function is introduced in a new formulation named Block Diagonal Hessian (BDH) method. Secondly, the BDH method is applied to the simultaneous spaceplane design and trajectory optimization problem, where the best size and its optimal trajectory are estimated to realize it. Through the several calculations, it is confirmed that the proposed BDH method is effective for simultaneous design and control optimization problems.

Journal

• Aeronautical and Space Sciences Japan

  Aeronautical and Space Sciences Japan 46 (533), 346-353, 1998

  THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Keywords

• Guidance and Control
• Simultaneous Optimization
• Nonlinear Programming
• Spaceplane

Details

• CRID: 1390282679456192640
• NII Article ID: 10002862870
• NII Book ID: AN00189072
• DOI: 10.2322/jjsass1969.46.346
• ISSN: 24241369
• ISSN: 00214663
• ISSN: http://id.crossref.org/issn/00214663
• NDL BIB ID: 4484521
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I4484521
• Web Site: https://www.jstage.jst.go.jp/article/jjsass1969/46/533/46_533_346/_pdf
• Text Lang: ja
• Data Source:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• Abstract License Flag: Disallowed