High Acceleration Cockpit Controller Locations. Volume 2. Test Plan
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1975
- Accession Number
- ADA014811
Entities
People
- C. F. Asiala
- S. L. Loy
Organizations
- McDonnell Aircraft Corporation