Paper
26 September 2007 Design optimization of a dual mode multi-axis passive isolation configuration for MLCD
Author Affiliations +
Abstract
A multi-axis passive isolation system was designed for dual mode operation to minimize pointing error due to spacecraft dynamic disturbances and to minimize payload response due to launch loads for the Mars terminal as part of the Mars Laser Communications Demonstration Project. Numerical optimization techniques using MSC/Nastran finite element software were utilized to explore isolator design configurations using a lower bound frequency constraint of 20 Hz subject to performance and mounting constraints. Response functions were developed that included the frequency spread of the six isolator modes and the rigid-body line-of-sight error due to translational and angular base disturbances that served as merit functions and/or constrained quantities during optimization. The performance of the resulting isolator configurations based on single and six degree-of-freedom isolator models are discussed.
© (2007) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Keith B. Doyle "Design optimization of a dual mode multi-axis passive isolation configuration for MLCD", Proc. SPIE 6665, New Developments in Optomechanics, 66650G (26 September 2007); https://doi.org/10.1117/12.732746
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Optical isolators

Mars

Passive isolation

Space operations

Computer aided design

Performance modeling

Received signal strength

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