Six-Axis Vibration Isolation Technology Applied to Spaceborne Interferometers
This paper discusses the vibration isolation problem as it applies to spaceborne
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This paper discusses the vibration isolation problem as it applies to spaceborne
This paper presents initial results that demonstrate the end-to-end operation of the Micro-Precision
This paper describes a disturbance analysis of the preliminary POINTS spacecraft and instrument design in order to determine whether and to what extent any isolation and/or added structural damping is necessary to meet the POINTS instrument requirements.
This paper is based on a collection of lessons-learned based on related missions including StarLight, a formation-flying stellar interferometry mission that merged with the Terrestrial Planet Finder technology development program just prior to entering phase C/D, the Space Interferometry Mission (currently in phase A), and the Shuttle Radar Topography Misssion of 2000.
A new technique of rotation shearing interferometry has been developed, which is optimized to reduce systematic problems when imaging through turbulence.
Several methods for mode shape expansion are investigated. In the first, the dynamic equations of motions are used to obtain direct solutions to the expanded eigenvectors. It is shown that these methods can be interpreted as constrained optimization problems.
Spaceborne optical interferometry has been idenfified as a critial technology for many of NASA's 21st century sceince visions.
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