摘要:
A high acceleration cockpit/controller design and integration program was conducted, using a full scale design aid. Alternate cockpit/controller configurations were developed for comparison using this full scale design aid in a fo...
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A high acceleration cockpit/controller design and integration program was conducted, using a full scale design aid. Alternate cockpit/controller configurations were developed for comparison using this full scale design aid in a formally structured evaluation including mission related task elements. Crew station and controller characteristics were thus related to operator needs in a mission context for advanced fighter concepts. (Author)
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