High Acceleration Cockpits for Advanced Fighter Aircraft. Volume IV. Test Results.
Abstract
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1974
- Accession Number
- AD0783603
Entities
People
- Carl F. Asiala
- Thomas J. Quinn
Organizations
- McDonnell Douglas