Micro-Precision Interferometer: Pointing System Performance in On-orbit Disturbance Environment
We investigate how the Space Interferometry Mission (SIM) will be able to meet its instrument astrometric pointing requirements.
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We investigate how the Space Interferometry Mission (SIM) will be able to meet its instrument astrometric pointing requirements.
This paper focuses specifically on passive structural damping with the goal to lower the control demand on active optics.
The proposed New Millenium Interferometry consists of three spacecraft separated by up to several kilometers. A heterodyne laser metrology system is proposed to measure the relative distances between the spacecraft.
A key thrust of NASA's Origins program is the search for and detection of planetary systems about other stars.
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Two different design methods for a networked constellation of N small satellites are presented. In the first method, the (linear) Clohessy-Wilthsire equations are used as an initial design tool, followed by conversion to a two-body model. Discrepancies between the linear and nonlinear solutions are minimized in the conversion process. The second method utilizes invariant manifold theory, by perturbing a reference trajectory in different directions along the center eigenvectors. Both methods require 5N parameters to fully define a constellation. In a relative, rotating frame of the reference path, the spacecraft appear as periodic ellipses of varying sizes. Deployment, reconfiguration using propulsive maneuvers, and station keeping costs for an example mission scenario are addressed.
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