Attitude control requirements for future space systemsLandsat-D and the Large Space Telescope represent current state-of-the-art systems with precise requirements placed on attitude control. Future systems for planetary stations, high precision earth monitoring and large precision deployable and erectable platforms project still more severe constraints and requirements on attitude control, including the requirement for many enabling and highly enhanced technologies beyond current state of the art. Two trend projections are identified for the areas of (1) precision pointing systems for earth orbiters and planetary spacecraft and (2) onboard high-capacity fast controllers for distributed control systems.
Document ID
19790050754
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Dahlgren, J. B. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Edmunds, R. S. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-0951Report Number: AIAA PAPER 79-0951
Meeting Information
Meeting: Conference on Advanced Technology for Future Space Systems