NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
On the attitude motion of a self-excited rigid bodyLeimanis (1965) has published a monograph, which contains Boedewadt's solution of Euler's equations of motion for a symmetric rigid body subject to a time-independent, self-excitement in a body-fixed direction. In addition, the monograph provided also Boedewadt's solution for the corresponding angles of rotation. It is pointed out that the solution of Euler's equations of motion provides a poor approximation to the problem of nearly symmetric rigid bodies in cases in which a high degree of accuracy (less than 1 percent error) is required. A much more accurate approximate solution has been provided by Longuski (1980). The result given by Leimanis in the case of the Eulerian angles is incorrect for arbitrary constant torques. The approximate solution given by Longuski, however, is extremely accurate and suitable for computer design work and error analysis of spacecraft performance. The present investigation is concerned with a review of the solutions and the specific regions of validity of the solution for the Eulerian angles.
Document ID
19850036522
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Longuski, J. M.
(California Institute of Technology, Jet Propulsion Laboratory, Mission Design Section, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1984
Publication Information
Publication: Journal of the Astronautical Sciences
Volume: 32
ISSN: 0021-9142
Subject Category
Astrodynamics
Accession Number
85A18673
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available