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Improved pointing at trackable targets by integrating control valve signalsA compact, low-cost add-on electronic module has been developed for the STRAP III control system to improve pointing at trackable targets. The module provides peak-to-peak limit cycle excursions of + or - 5 arcseconds while tracking a +3 magnitude or brighter star. This is achieved without using rate-integrating gyroscopes, thus reducing payload length, weight, cost, and preparation time. This module has flown successfully five times. In May 1981, it improved the performance of a two-startracker attitude control system with TV camera and joystick control which pointed at a nontrackable target. This paper describes the operation of the module, how it alters the ordinary STRAP III operation, and how it was developed using an analog-computer-based rocket flight simulator.
Document ID
19820064513
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Stone, R. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Laverty, C. R.
(NASA Goddard Space Flight Center Special Payloads Div., Greenbelt, MD, United States)
Colby, M. J.
(GE Management and Technical Services Co. Lanham, MD, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 82-1738
Meeting Information
Meeting: Sounding Rocket Conference
Location: Orlando, FL
Start Date: October 26, 1982
End Date: October 28, 1982
Accession Number
82A48048
Distribution Limits
Public
Copyright
Other

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