Evaluation of AFIT/F-16 Restraint Concepts in the + or - 2Gy Environment
Abstract
The acceleration stresses imposed by the lateral (+ or - Gy) maneuvering capabilities of six-degrees-of-freedom (6DOF) aircraft, such as the AFTI/F-16, may potentially impact pilot performance. This centrifuge research was done to evaluate the effectiveness of special canopy-rail-mounted shoulder restraints at + or - Gy in the presence of a sum-of-sines tracking task implemented via a side stick (force) controller. Results indicate that additional restraints are desirable.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1980
- Accession Number
- ADA094323
Entities
People
- Dana B. Rogers
- Daniel W. Repperger
- John W. Frazier
- Robert E. Van Patten
Organizations
- Air Force Research Laboratory