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A computer-aided telescope pointing system utilizing a video star trackerThe Video Inertial Pointing (VIP) System developed to satisfy the acquisition and pointing requirements of astronomical telescopes is described. A unique feature of the system is the use of a single sensor to provide information for the generation of three axis pointing error signals and for a cathode ray tube (CRT) display of the star field. The pointing error signals are used to update the telescope's gyro stabilization and the CRT display is used by an operator to facilitate target acquisition and to aid in manual positioning of the telescope optical axis. A model of the system using a low light level vidicon built and flown on a balloon-borne infrared telescope is briefly described from a state of the art charge coupled device (CCD) sensor. The advanced system hardware is described and an analysis of the multi-star tracking and three axis error signal generation, along with an analysis and design of the gyro update filter, are presented. Results of a hybrid simulation are described in which the advanced VIP system hardware is driven by a digital simulation of the star field/CCD sensor and an analog simulation of the telescope and gyro stabilization dynamics.
Document ID
19760011132
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Murphy, J. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Lorell, K. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Swift, C. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-73079
A-6365
Report Number: NASA-TM-X-73079
Report Number: A-6365
Accession Number
76N18220
Funding Number(s)
PROJECT: RTOP 506-19-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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