Systems consist of single duct system with two sets of reaction control nozzles, one linked mechanically to pilot's controls, and other set driven by electric servomotors commanded by preselected combinations of electrical signals.
Attitude controls for VTOL aircraft
1971-06-01
Miscellaneous
No indication
English
Attitude controls for VTOL aircraft Patent
NTRS | 1969
|Tailsitter VTOL flying wing aircraft attitude control
IEEE | 2016
|Reaction controls for jet-lift VTOL aircraft
AIAA | 1969
|Jet engine control and attitude control in vertical attitude VTOL aircraft
Engineering Index Backfile | 1958
|JET ENGINE CONTROL AND ATTITUDE CONTROL IN VERTICAL ATTITUDE VTOL AIRCRAFT
SAE Technical Papers | 1958
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