Share Email Print

Proceedings Paper

Structural line-of-sight jitter analysis for MLCD
Author(s): Keith B. Doyle
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

A central aspect in the design of the Mars lasercom terminal was limiting the line-of-sight jitter of the optical payload due to translational and angular dynamic excitation from the host spacecraft. Line-of-sight jitter analyses were performed on the Mars terminal payload that accounted for the passive and active stabilization systems, the elastic response of the payload, and the detailed elastic characteristics of the isolator. The line-of- jitter was significantly impacted by the coupling between the local dynamic response of the isolator main spring and the payload structure. Critical modes of the payload are identified and the impact of the isolator main spring surge mode is discussed along with mitigation strategies using models correlated to vibration test data.

Paper Details

Date Published: 26 September 2007
PDF: 12 pages
Proc. SPIE 6665, New Developments in Optomechanics, 66650I (26 September 2007); doi: 10.1117/12.732763
Show Author Affiliations
Keith B. Doyle, MIT Lincoln Lab. (United States)

Published in SPIE Proceedings Vol. 6665:
New Developments in Optomechanics
Alson E. Hatheway, Editor(s)

© SPIE. Terms of Use
Back to Top