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Spacecraft drag-free technology development: On-board estimation and control synthesisEstimation and control methods for a Drag-Free spacecraft are discussed. The functional and analytical synthesis of on-board estimators and controllers for an integrated attitude and translation control system is represented. The framework for detail definition and design of the baseline drag-free system is created. The techniques for solution of self-gravity and electrostatic charging problems are applicable generally, as is the control system development.
Document ID
19820021476
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Key, R. W. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mettler, E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Milman, M. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Schaechter, D. B. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 15, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JPL-Pub-82-45
NAS 1.26:169141
NASA-CR-169141
Report Number: JPL-Pub-82-45
Report Number: NAS 1.26:169141
Report Number: NASA-CR-169141
Accession Number
82N29352
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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