In an effort to achieve maximum aircraft performance, designers are integrating aircraft systems. The characteristics of aerodynamics, vehicle structure, and propulsion systems are being integrated and controlled through embedded, often flight-critical, electronic systems. This paper addresses the qualification needs for such highly integrated aircraft systems. Based on flight experience with research aircraft, a set of test capabilities is described which allows for complete and efficient qualification of advanced integrated aircraft.
Qualification needs for advanced integrated aircraft
Guidance, Navigation and Control Conference ; 1985 ; Snowmass, CO
1985-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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