NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Reactionless gimbal actuator for precision pointing of large payloadsA novel actuator for application to precision pointing gimbal systems is described. The new actuator, dubbed the Reactuator, is capable of large output torques for payload pointing while minimizing reaction torques that can excite gimbal support structure. The Reactuator is able to approach reactionless operation by using an integral wheel to absorb the reaction torques. The advantages that result are described through analysis and simulation examples. Methods for designing control algorithms for the Reactuator are discussed and the results of preliminary breadboard tests are presented.
Document ID
19890025320
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Laskin, R. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kopf, E. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sirlin, S. W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Spanos, J. T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wiktor, P. J.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 87-512
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Kalispell, MT
Country: United States
Start Date: December 6, 1987
End Date: December 9, 1987
Sponsors: AIAA, AAS
Accession Number
89A12691
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available