A two-pulse scheme for the time-optimal attitude control of a spinning missile
Guidance, Navigation and Control Conference ; 1990 ; Portland , OR , U.S.A.
1990-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Time-Optimal Attitude Control Scheme for a Spinning Missile
Online Contents | 1993
|Time-Optimal Attitude Control of a Spinning Vehicle
NTIS | 1967
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