Design and deployment of a satellite constellation using collaborative optimization

被引:43
作者
Budianto, IA [1 ]
Olds, JR [1 ]
机构
[1] Georgia Inst Technol, Sch Aerosp Engn, Space Syst Design Lab, Atlanta, GA 30332 USA
关键词
Algorithms - Convergence of numerical methods - Infrared radiation - Optimization - Parameter estimation - Problem solving;
D O I
10.2514/1.14254
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A study of collaborative optimization as a systematic, multivariable, multidisciplinary method for the conceptual design of satellite constellations is presented. Collaborative optimization was selected because it is well suited to a team-oriented environment, such as often found in the constellation design process. The method provides extensive and formal exploration of the multidisciplinary design space and a scalable formulation of the problem without compromising its subsystems' flexibility or eliminating opportunities for collaboration. The feasibility and benefits of the collaborative optimization architecture are highlighted by the successful convergence of an application notional problem to design and deploy elements of a space-based infrared system that provides early missile warning. Furthermore, this study contributes to the existing knowledge of the collaborative optimization method by verifying the feasibility of nongradient optimization algorithms as both system and subsystem optimizers within the architecture. Finally, the demonstrated convergence of this problem, which involves integer variables, also demonstrates the flexibility of the architecture for handling mixed-discrete nonlinear multidisciplinary problems.
引用
收藏
页码:956 / 963
页数:8
相关论文
共 29 条
[1]  
*AIAA TECHN COMM, 1991, CURR STAT ART MULT D
[2]  
BRAUN RD, 1996, THESIS U STANDFORD D
[3]  
BUDIANTO IA, 2000, THESIS GEORGIA I TEC
[4]  
CANAN JW, 2000, AEROSPACE AM MAY, P35
[5]  
*COMM SPAC TRANSP, 1998, 1998 YEAR REV ASS AD, P9
[6]  
ELY TA, 1998, 98128 AAS
[7]   Systems engineering trades for the IRIDIUM(R) constellation [J].
Garrison, TP ;
Ince, M ;
Pizzicaroli, J ;
Swan, PA .
JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (05) :675-680
[8]  
GEORGE E, 1997, 97621 AAS
[9]   METHOD FOR NONLINEAR MIXED-INTEGER PROGRAMMING AND ITS APPLICATION TO DESIGN PROBLEMS [J].
GISVOLD, KM ;
MOE, J .
JOURNAL OF ENGINEERING FOR INDUSTRY, 1972, 94 (02) :353-+
[10]  
HOULT CP, 1999, P 1999 IEEE AER C IE, V4, P209