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Simulation validation of the XV-15 tilt-rotor research aircraft (1984)

Churchill, G. B. ; Hanson, G. D. ; Ferguson, S. W.

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Publication Date: 2018-12-01

Description: The results of a simulation validation program of the XV-15 tilt-rotor research aircraft are detailed, covering such simulation aspects as the mathematical model, visual system, motion system, cab aural system, cab control loader system, pilot perceptual fidelity, and generic tilt rotor applications. Simulation validation was performed for the hover, low-speed, and sideward flight modes, with consideration of the in-ground rotor effect. Several deficiencies of the mathematical model and the simulation systems were identified in the course of the simulation validation project, and some were corrected. It is noted that NASA's Vertical Motion Simulator used in the program is an excellent tool for tilt-rotor and rotorcraft design, development, and pilot training.

Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE

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