Load Relief Control of H-IIA Launch Vehicle
16th, IFAC symposium on automatic control in aerospace ; 2004 ; St. Petersburg, Russia
2004-01-01
6 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Load relief control of launch vehicle using aerodynamic angle estimation
SAGE Publications | 2018
|Control Enhanced and Parameterized Load Relief Technology for a Launch Vehicle
British Library Conference Proceedings | 2015
|