Approaches for further rationalisation in mechanical architecture and structural design of satellites

H. Baier; T. Pühlhofer

Approaches for further rationalisation in mechanical architecture and structural design of satellites

H. Baier, T. Pühlhofer

Engineering and Design

Technical University of Munich

Research output: Contribution to conference › Paper › peer-review

7 Scopus citations

Abstract

CAE based approaches for supporting the definition and in part also further detailization of geometrical and mechanical architecture of satellites are discussed. Related methods based on different techniques such as optimization including genetic algorithm are presented. Emphasis is put on demonstration and verification with practical examples such as positioning of equipment on panels including panel design, as well as a full satellite structure. Experience shows that problem statements have to be quite complete, and especially for total satellites proper decomposition into subtasks is required.

Original language	English
Pages	1513-1519
Number of pages	7
State	Published - 2003
Event	54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law - Bremen, Germany Duration: 29 Sep 2003 → 3 Oct 2003

Conference

Conference	54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law
Country/Territory	Germany
City	Bremen
Period	29/09/03 → 3/10/03

Keywords

Configuration design
Genetic algorithm
Mechanical architecture
Optimization
Satellite design

Cite this

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title = "Approaches for further rationalisation in mechanical architecture and structural design of satellites",

abstract = "CAE based approaches for supporting the definition and in part also further detailization of geometrical and mechanical architecture of satellites are discussed. Related methods based on different techniques such as optimization including genetic algorithm are presented. Emphasis is put on demonstration and verification with practical examples such as positioning of equipment on panels including panel design, as well as a full satellite structure. Experience shows that problem statements have to be quite complete, and especially for total satellites proper decomposition into subtasks is required.",

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author = "H. Baier and T. P{\"u}hlhofer",

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note = "54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law ; Conference date: 29-09-2003 Through 03-10-2003",

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Baier, H & Pühlhofer, T 2003, 'Approaches for further rationalisation in mechanical architecture and structural design of satellites', Paper presented at 54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law, Bremen, Germany, 29/09/03 - 3/10/03 pp. 1513-1519.

Approaches for further rationalisation in mechanical architecture and structural design of satellites. / Baier, H.; Pühlhofer, T.
2003. 1513-1519 Paper presented at 54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law, Bremen, Germany.

Research output: Contribution to conference › Paper › peer-review

TY - CONF

T1 - Approaches for further rationalisation in mechanical architecture and structural design of satellites

AU - Baier, H.

AU - Pühlhofer, T.

PY - 2003

Y1 - 2003

N2 - CAE based approaches for supporting the definition and in part also further detailization of geometrical and mechanical architecture of satellites are discussed. Related methods based on different techniques such as optimization including genetic algorithm are presented. Emphasis is put on demonstration and verification with practical examples such as positioning of equipment on panels including panel design, as well as a full satellite structure. Experience shows that problem statements have to be quite complete, and especially for total satellites proper decomposition into subtasks is required.

AB - CAE based approaches for supporting the definition and in part also further detailization of geometrical and mechanical architecture of satellites are discussed. Related methods based on different techniques such as optimization including genetic algorithm are presented. Emphasis is put on demonstration and verification with practical examples such as positioning of equipment on panels including panel design, as well as a full satellite structure. Experience shows that problem statements have to be quite complete, and especially for total satellites proper decomposition into subtasks is required.

KW - Configuration design

KW - Genetic algorithm

KW - Mechanical architecture

KW - Optimization

KW - Satellite design

UR - http://www.scopus.com/inward/record.url?scp=22344433306&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:22344433306

SP - 1513

EP - 1519

T2 - 54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law

Y2 - 29 September 2003 through 3 October 2003

ER -

Approaches for further rationalisation in mechanical architecture and structural design of satellites

Abstract

Conference

Keywords

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