Adjustable simulation vehicle capabilities

Data processing: structural design – modeling – simulation – and em – Simulating nonelectrical device or system – Mechanical

Reexamination Certificate

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Details

C434S037000, C244S191000, C244S203000

Reexamination Certificate

active

07146299

ABSTRACT:
The present invention is a system and method for easily adjusting flight characteristics of a simulated aircraft. The system allows a user to adjust commanded pitch, roll or yaw values or steady state frequency response values that are associated with an atmospheric temperature value, an atmospheric dynamic pressure value, aileron position, rudder position, and elevator position.

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Stevenson et al., “Real time aircraft simulation using J-Mass”, IEEE 1995.

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