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Simulation requirements for the Large Deployable Reflector (LDR)Simulation tools for the large deployable reflector (LDR) are discussed. These tools are often the transfer function variety equations. However, transfer functions are inadequate to represent time-varying systems for multiple control systems with overlapping bandwidths characterized by multi-input, multi-output features. Frequency domain approaches are the useful design tools, but a full-up simulation is needed. Because of the need for a dedicated computer for high frequency multi degree of freedom components encountered, non-real time smulation is preferred. Large numerical analysis software programs are useful only to receive inputs and provide output to the next block, and should be kept out of the direct loop of simulation. The following blocks make up the simulation. The thermal model block is a classical heat transfer program. It is a non-steady state program. The quasistatic block deals with problems associated with rigid body control of reflector segments. The steady state block assembles data into equations of motion and dynamics. A differential raytrace is obtained to establish a change in wave aberrations. The observation scene is described. The focal plane module converts the photon intensity impinging on it into electron streams or into permanent film records.
Document ID
19840024247
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Soosaar, K.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1984
Subject Category
Astronomy
Report/Patent Number
NASA-CR-171140
NAS 1.26:171140
CSDL-R-1725
Report Number: NASA-CR-171140
Report Number: NAS 1.26:171140
Report Number: CSDL-R-1725
Accession Number
84N32317
Funding Number(s)
CONTRACT_GRANT: NAS8-34904
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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