Proposal for powered control system for aircraft
Proposal for powered control system for aircraft
- Neue Suche nach: Price, H.L.
- Neue Suche nach: Price, H.L.
System features safeguards against power failure, together with complete integration with automatic pilot; failure of servo power supply automatically introduces additional aero-dynamic aid sufficient for emergency conditions, without undue piloting fatigue; "feel" is available to any desired degree under power assistance, and follows spring tab law of variation with speed; servo motor may replace autopilot, thus effecting automatic trimming of servo load.
Dokumentinformationen
Proposal for powered control system for aircraft
Aircraft Eng
Aircraft Engineering ; 21 , n 247
1949
6 pages
Aufsatz (Zeitschrift)
Englisch
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