Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stability and performance of closed loop system
Minimax attitude control of aeroballistic launch vehicles
1965-12-01
Report
No indication
English
Minimax attitude control of aeroballistic launch vehicles
Engineering Index Backfile | 1965
In-Tube Catapult Launch from Rectangular-Bore Aeroballistic Range
Online Contents | 2015
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