High Acceleration Cockpits for Advanced Fighter Aircraft. Volume IV. Test Results.

摘要

A high acceleration cockpit design test/evaluation program was conducted,using a full scale design aid. Alternate configurations were compared using this full scale design aid in a formally structured evaluation including mission related task elements. Test criteria considered evaluation of control/display and cockpit design options,including seat location,motion,and pilot anthropometry,with a balance between the physical and operational test measures and objectives using Air Force provided pilot subjects. (Author)