Helicopter cockpit intersection data design and rapid verification method

Abstract

The invention belongs to the technical field of helicopter man-machine work efficiency, and particularly relates to a helicopter cockpit intersection point data design and rapid verification method, which comprises the following steps of: 1, designing cockpit intersection point data, namely determining a design eye position point of a driver, determining intersection point data of a driver seat and determining intersection point data of a driver joystick; determining intersection point data of a driver total distance rod, determining intersection point data of driver pedals, determining intersection point data of a central control board, and determining intersection point data of an instrument board; and 2, verifying the cockpit intersection data designed in the step 1 based on the variable configuration cockpit platform, namely setting the cockpit intersection data based on the variable configuration cockpit platform, scoring the cockpit intersection data by adopting an expert scoring method, and returning the intersection data which does not meet the requirement to the step 1 for optimization.

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