Ground Transfer Alignment and IMU Acceleration and Rate Biases Estimation Using Launcher's Attitude Only at Three Static Angular Poses of the Launcher
53rd, Israel annual conference on aerospace sciences ; 2013 ; Tel-Aviv, Israel
2013-01-01
6 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Impact of Ice during Launcher's Ascent
AIAA | 2011
|Estimation of Vehicle Attitude using Three-Axis Acceleration and Two-Axis Angular Velocity
British Library Conference Proceedings | 2009
|Satellite Launcher Attitude Tracking and Normal Acceleration Regulation Control Law
British Library Conference Proceedings | 2000
|Estimation of Attitude Sensor Timetag Biases
British Library Conference Proceedings | 1995
|