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Pointing control for LDROne important aspect of the LDR control problem is the possible excitations of structural modes due to random disturbances, mirror chopping, and slewing maneuvers. An analysis was performed to yield a first order estimate of the effects of such dynamic excitations. The analysis involved a study of slewing jitters, chopping jitters, disturbance responses, and pointing errors, making use of a simplified planar LDR model which describes the LDR dynamics on a plane perpendicular to the primary reflector. Briefly, the results indicate that the command slewing profile plays an important role in minimizing the resultant jitter, even to a level acceptable without any control action. An optimal profile should therefore be studied.
Document ID
19900004137
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yam, Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Briggs, C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 15, 1988
Publication Information
Publication: Report of the Asilomar 3 LDR Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N13453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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