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24 September 2011Design and verification of a robust secondary mirror adjustable supporting mechanism for airborne optical remote sensing instruments
This work presents a developing design of adjustable supporting mechanism of secondary mirror for airborne Cassegrain
optical remote sensing instruments. Several datum surfaces and shims have been designed in this mechanism, shims and
one of structural parts can be released and are properly grinded to the desired thickness. The proposed mechanism has
been verified by an experimental model. The reassembled accuracy is 5 arcsecond and ±3 μm for orientation and position
respectively. Furthermore, their adjustable accuracy can achieve 5 arcsecond and ±3 μm respectively, depending on
grinding and measurement precision. The accuracy can drive the optical system performance to design specification.
After verification, we confirm the proposed design of adjustable supporting mechanism can be applied to airborne
Cassegrain optical systems, and has good potential in spaceborne applications.
Po-Hsuan Huang,Yu-Cheng Cheng, andShenq-Tsong Chang
"Design and verification of a robust secondary mirror adjustable supporting mechanism for airborne optical remote sensing instruments", Proc. SPIE 8125, Optomechanics 2011: Innovations and Solutions, 812511 (24 September 2011); https://doi.org/10.1117/12.893202