Simulation of aircraft using airborne V/STOL simulator is described; program was undertaken to assess influence on handling qualities of backlash and flexibility in various locations in control systems, and various realistic stability augmentation failures in presence of these backlashes; tests were completed before actual aircraft flew and, in addition to providing Canadair with data on backlashes, familiarized company pilots with flying and control system characteristics to be expected.
Simulation of Canadair CL-84 tilt-wing aircraft using airborne V/STOL simulator
Canada. Nat Research Council -- Aeronautical Report
1965
33 pages
Report
Englisch
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