Flexible Launch Vehicle Attitude Control Design Using Coevolutionary Algorithm
16th, IFAC symposium on automatic control in aerospace ; 2004 ; St. Petersburg, Russia
2004-01-01
6 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Launch vehicle attitude control
NTRS | 1975
NOVEL ATTITUDE CONTROL DESIGN OF SPACE LAUNCH VEHICLE
TIBKAT | 2021
|Launch Vehicle Attitude Control Using Higher-Order Sliding Modes
British Library Conference Proceedings | 2010
|