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Predicting a vehicle's attitude response to a single yo despinThe method developed for analysis of single yo despin systems is a two step process. The first step utilizes the despin equations for a yo or yo-yo system to compute the cable tension force and its point of application on the body throughout the despin process. The second step considers the actual body configuration and treats the force just discussed as a prescribed external force acting on the surface of the body at the physical location of the despin system. The resulting vehicle coning angle is first computed using a digital computer program for a body with no initial coning prior to despin. Closed form solutions which utilize the previous results are then used to treat the effects of initial conditions.
Document ID
19760052774
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bensimon, M.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-1853
Meeting Information
Meeting: Sounding Rocket Technology Conference
Location: Boston, MA
Start Date: June 23, 1976
End Date: June 25, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A35740
Distribution Limits
Public
Copyright
Other

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