Vertically oriented satellites instrumenting orbital plane exhibit certain gyroscopic properties; if one or more integrating gyroscopes are properly installed, characteristic may be used to accomplish semipassive damping of vehicle librations; vehicle oscillations cause gimbal precession in gyroscopes; damping occurs because of energy dissipation as heat in viscous restraint of each gyro; systems described comprise only gyro or gyros, properly supplied with constant power; neither external error sensing nor on-board computation is required.
Attitude control of satellites using integrating gyroscopes
Am Astronautical Soc -- Advances Astronautical Sciences
1962
28 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Three-Axis Attitude Estimation Using Rate-Integrating Gyroscopes
Online Contents | 2016
|Controllability of spacecraft attitude using control moment gyroscopes
Tema Archiv | 2009
|