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TruVision™ visual system with 220° horizontal x 60° vertical field
of view
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Highly
detailed database
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Simulated EFIS and VEMD displays
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Flight
test validation data
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Automatic certification testing
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Electric control loading
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Multi-channel sound simulation
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NVG
compatibility
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Frasca’s Auto-test Utility. This consists of software
and sensors, which automatically fly the FTD though the required JAA
maneuvers, record its performance and allow the FTD’s performance to be
compared to flight test data from the aircraft.
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Blade Element Modeling
techniques (BEMT)-analyzes the airflow over the rotor by dividing the
rotor into small segments. Each segment is analyzed continuously as the blade
moves through the air. The individual forces of each segment are then summed
to determine the net forces that act in the simulation. Blade element
modeling offers superior performance to disk models that treat the entire
rotor disk as a single element. Disk models require extensive software to
deal with special conditions such as retreating blade stall, settling with
power and autorotation. These conditions are simulated without special
consideration when using blade element modeling.
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Cockpit
controls connected to precision electric actuators in order to provide
realistic forces as encountered in flight.
