Automatic Flight Control Development for General Aviation
Automatic Flight Control Development for General Aviation
- New search for: Vetter, Lee J.
- New search for: Vetter, Lee J.
A fluidic flight control system has been flight tested to develop and evaluate vortex rate sensors, fluidic amplifiers, dynamic shaping techniques, and system accuracy. Discussed are results which have confirmed applicability of conventional control theory and projected high reliability. Also discussed is a stabilization system featuring an electropneumatic servo actuator with variable transfer function and unique characteristics for application to a range of stabilization problems. Recent electronic system studies have shown substantial improvement in reliability, maintainability, size, weight, and cost reduction by use of microelectronic functional modules as alternates to individually-mounted discrete components.
Document information
Automatic Flight Control Development for General Aviation
Sae Technical Papers
3rd Annual Business Aircraft Conference (1967) ; 1967
1967-02-01
Conference paper
English
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