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- W2187101888 abstract "A joint program between NLX Corporation, Virginia, USA and the Flight Research Laboratory (FRL) of Canada’s National Research Council (NRC) was initiated to develop a high fidelity simulator mathematical model for the Raytheon King Air 350 business aircraft (Fig. 1). The flight-test data, as well as the aerodynamic model developed from the data, conformed to JAA’s Level-D Simulator data standards [1] and IATA’s Flight Simulator Design and Performance Data Requirements [2]. Efficient data system architecture, in terms of both software algorithms and hardware processing, has been employed to meet the stringent requirements of a Level-D simulator mathematical model. Additionally, novel hardware and software techniques have been applied to the calibration and measurement of the fundamental in-flight parameters such as air data. The small perturbation stability and control derivatives were formulated versus parameters such as Mach, alpha, beta, thrust and flap setting to develop a global model of the aircraft. The flight data used for model validation conformed to the FAA’s Qualification Test Guide (QTG) manoeuvres specifications [3]. This program has clearly demonstrated major improvements in the efficiency and time required to develop a simulator mathematical model for a fixed wing aircraft, from flight-test data." @default.
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- W2187101888 date "2002-01-01" @default.
- W2187101888 modified "2023-09-27" @default.
- W2187101888 title "KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC MODEL DEVELOPMENT" @default.
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