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STRAP V - Higher accuracy, lower drift attitude control systemThe STRAP V system was developed to provide higher accuracy and lower limit cycle fine pointing (+ or - 7 arcseconds) in all three axes at targets which cannot be tracked by startrackers or solar trackers. The system provides an increase in pointing performance over that obtainable with the STRAP IV (1) Attitude Control System (ACS). The STRAP IV concept of third axis updates is utilized to reduce pointing errors, using the flight-proven STRAP III (2) system as a first stage. Flight aspect photographs and telemetry records show that the STRAP V objectives have been met. The STRAP IV major error contributors have been significantly reduced and the tracking flexibility has been increased with only minor error contributions. Attention is given to the basic STRAP III control modes, major STRAP IV system error sources, tuned restrained inertial gyros (TRIGs), the programmable sequence timer, the STRAP V control box, third axis update, system gyro alignments, and STRAP V operational capabilities.
Document ID
19820064506
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Budney, T. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Collinson, T. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Stone, R. W.
(NASA Goddard Space Flight Center Special Payloads Div., Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-1731
Report Number: AIAA PAPER 82-1731
Meeting Information
Meeting: Sounding Rocket Conference
Location: Orlando, FL
Start Date: October 26, 1982
End Date: October 28, 1982
Accession Number
82A48041
Distribution Limits
Public
Copyright
Other

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