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Precision pointing and tracking system /PPTS/As part of its advanced development work, JPL is developing a Precision Pointing and Tracking System (PPTS) for science platform control on unmanned planetary spacecraft. The PPTS will extend science capabilities on future missions by providing highly accurate (10 arcsec) and stable (0.2 arcsec) pointing of the platform. Key features of the design include closed-loop tracking of target bodies using an optical sensor and decoupling of spacecraft dynamics via high-bandwidth, inertially stabilized control. This paper discusses the analyses and design. Computer simulations were used to establish the feasibility of the design approach and to verify that the performance requirements can be met. A breadboard demonstration of the entire system is expected in late 1980.
Document ID
19780060474
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, T. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Leblanc, D. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mettler, E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gaalema, S. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1978
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 78-114
Meeting Information
Meeting: Annual Rocky Mountain Guidance and Control Conference
Location: Keystone, CO
Start Date: March 10, 1978
End Date: March 13, 1978
Sponsors: American Astronautical Society
Accession Number
78A44383
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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