Paper
3 June 1987 The Design Of A Space Optical System Using Computer-Aided Engineering Techniques
Gareth R. Thomas, Ralph D. Brillhart, Edmund A. Louie
Author Affiliations +
Proceedings Volume 0748, Structural Mechanics of Optical Systems II; (1987) https://doi.org/10.1117/12.939815
Event: OE LASE'87 and EO Imaging Symposium, 1987, Los Angeles, CA, United States
Abstract
Using computer-aided engineering (CAE) tools and techniques for the design of a space optical system, from preliminary design through testing of hardware, provided an excellent means for compressing project schedules. The three principal steps in the process were (1) solids modeling, (2) structural analysis, and (3) design test. Geometric solid modeling requires that the components of the system be described expli-citly in the CAE database. In this case the components consist of a number of electronic chassis and their associated circuit boards, the optical head, the gimballed mirror and the optical bench. The CAE database was used to support: (a) checks of layouts and parts interference, (b) development and modification of designs, (c) fabrication drawing preparation, (d) computation of properties for further computer analysis, (e) project team communication, and (f) generation of presentation aids for customer communication.
© (1987) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Gareth R. Thomas, Ralph D. Brillhart, and Edmund A. Louie "The Design Of A Space Optical System Using Computer-Aided Engineering Techniques", Proc. SPIE 0748, Structural Mechanics of Optical Systems II, (3 June 1987); https://doi.org/10.1117/12.939815
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KEYWORDS
Solid modeling

Computer aided design

Mirrors

Databases

Structural analysis

Systems modeling

Electronic components

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