Integrated modeling for design of lightweight, active mirrors

被引:25
作者
Cohan, Lucy E. [1 ]
Miller, David W. [1 ]
机构
[1] MIT, Dept Aeronaut & Astronaut, Cambridge, MA 02139 USA
关键词
integrated model; lightweight mirrors; space telescope; active optics; LARGE SPACE STRUCTURES;
D O I
10.1117/1.3592520
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Lightweight, active, silicon carbide mirrors have the potential to enable larger primary aperture, space-based optical systems, hence improving the resolution and sensitivity of such systems. However, due to the lack of design heritage, the best mirror designs are not yet known. Therefore, an integrated model of the lightweight mirrors is created in order to explore the design space. The model determines the achievable radius of curvature change within wavefront error limits, the peak launch stress, and the mass of a mirror segment. However, designing a mirror to meet any of these individual objectives results in a system that performs poorly in terms of the other objectives. Therefore, a full trade space analysis is run to determine the portions of the design space that best balance the trade-offs between metrics. These results are used to determine designs that perform well with respect to specific missions and can be used for future mirror designs. (C) 2011 Society of Photo-Optical Instrumentation Engineers (SPIE). [DOI: 10.1117/1.3592520]
引用
收藏
页数:13
相关论文
共 18 条
[1]  
[Anonymous], 1987, Standard on Piezoelectricity
[2]  
Cochran W.G., 2007, Sampling techniques
[3]  
COHAN LE, 2010, AIAA ASME ASCE AHS A, pQ2980
[4]  
COHAN LE, 2010, THESIS MIT, pQ2980
[5]  
COHAN LE, 2011, OPT ENG, V50, pQ2980
[6]   USE OF PIEZOELECTRIC ACTUATORS AS ELEMENTS OF INTELLIGENT STRUCTURES [J].
CRAWLEY, EF ;
DELUIS, J .
AIAA JOURNAL, 1987, 25 (10) :1373-1385
[7]  
Ealey M. A., 2004, Proceedings of the SPIE - The International Society for Optical Engineering, V5166, P19, DOI 10.1117/12.512726
[8]   POSITIVE POSITION FEEDBACK-CONTROL FOR LARGE SPACE STRUCTURES [J].
FANSON, JL ;
CAUGHEY, TK .
AIAA JOURNAL, 1990, 28 (04) :717-724
[9]   Finite element modeling of composite piezoelectric structures with MSC/NASTRAN [J].
Freed, BD ;
Babuska, V .
SMART STRUCTURES AND INTEGRATED SYSTEMS - SMART STRUCTURES AND MATERIALS 1997, 1997, 3041 :676-688
[10]   ON THE STABILITY PROBLEM CAUSED BY FINITE ACTUATOR DYNAMICS IN THE COLLOCATED CONTROL OF LARGE SPACE STRUCTURES [J].
GOH, CJ ;
CAUGHEY, TK .
INTERNATIONAL JOURNAL OF CONTROL, 1985, 41 (03) :787-802