发明名称 Dynamic flight simulator control system
摘要 A dynamic flight simulator control system for enhancing flight realism to a pilot with regard to his perception and response to the linear forces and angular motions generated by a gimballed force and motion platform at the end of a rotating arm. Flight commands generated by controls identical to those in a specified aircraft and operated by the pilot as if flying are converted to the forces and motions predetermined for the aircraft and translated into simulator command signals which regulate the angular velocity of the arm and the roll and pitch of the platform. The perceived angular motions for both the aircraft pilot and the simulator pilot are predicted by computers pre-programmed with mathematical models of their human angular sensor responses and any difference is minimized by iteratively adjusting coefficients in the simulator command signals for predetermined weighting factors based on the individual pilot's preference.
申请公布号 US4751662(A) 申请公布日期 1988.06.14
申请号 US19860887418 申请日期 1986.07.14
申请人 UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 CROSBIE, RICHARD J.
分类号 G09B9/12;(IPC1-7):G09B9/08 主分类号 G09B9/12
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