Spacecraft Attitude and Rate Determination using Numerical Gyros (AIAA 2013-5022)
Conference, Guidance, navigation and control; AIAA guidance ; 2013 ; Boston, MA
2013-01-01
14 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Spacecraft Attitude Determination Using Electrostatically Suspended Gyros
British Library Conference Proceedings | 2002
|Spacecraft Attitude Rate Measurement Systems without Gyros
British Library Online Contents | 1997
|Spacecraft Attitude Determination Using Gyros and Quaternion Measurements
Online Contents | 1996
|