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Gyro motion boundedness under uncertain vehicle spin and accelerationUsing a quadratic Liapunov function, a condition is obtained for the boundedness of the motion of the gyro mounted in a vehicle which has a time-varying uncertain angular acceleration and deceleration omega-x(t) about the output axis, and is spinning with uncertain angular velocity omega-z(t) about the spin axis of the gyro. A region of ultimate boundedness in the theta-theta plane is obtained which the motion of the gyro eventually enters and in which it remains after a finite interval of time for any uncertain omega-x(t) and omega-z(t). The gyro motion is shown to be bounded if the uncertainty in the spin velocity does not exceed a certain threshold value. This condition disappears if omega-z(t) = 0.
Document ID
19840049507
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Singh, S. N.
(NASA Langley Research Center; Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1984
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-20
ISSN: 0018-9251
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
84A32294
Distribution Limits
Public
Copyright
Other

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