NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Analytic solutions for dual-spin spacecraft during platform motionThis paper presents analytic solutions to the dynamic equations of dual-spinners during platform slews. The rotor is assumed to be an axisymmetric balanced rigid body. The platform is an asymmetric rigid body with small static and dynamic imbalances. The solutions given in this paper extend a previous theory which provided an approximate solution only in the steady state.
Document ID
19840047803
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hayati, S. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hamidi, M. (California Institute of Technology, Jet Propulsion Laboratory, Automated Systems Section, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 83-410
Report Number: AAS PAPER 83-410
Accession Number
84A30590
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available