In recent efforts by NASA, the Army, and Advanced Rotorcraft Technology, Inc. (ART), the application of parallel processing techniques to real-time simulation have been studied. Traditionally, real-time helicopter simulations have omitted the modeling of high-frequency phenomena in order to achieve real-time operation on affordable computers. Parallel processing technology can now provide the means for significantly improving the fidelity of real-time simulation, and one specific area for improvement is the modeling of rotor dynamics. This paper focuses on the results of a piloted simulation in which a traditional rotor-map mathematical model was compared with a more sophisticated blade-element mathematical model that had been implemented using parallel processing hardware and software technology.
A comparison of real-time blade-element and rotor-map helicopter simulations using parallel processing
AHS, Annual Forum ; 1990 ; Washington, DC, United States
1990-01-01
Conference paper
No indication
English
Helicopter Rotor Disk and Blade Element Comparisons
British Library Conference Proceedings | 1996
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