FLIGHT MEASUREMENTS OF THE INFLUENCE OF SPEED STABILITY ON THE LANDING APPROACH,
Abstract
A small delta aircraft has been used to study the effects of speed instability on the pilot workload and accuracy in the approach task. Speed instability was produced by the use of a reversed autothrottle which varied thrust with airspeed and/or incidence. Glide path control was by radio talkdown, based on information from either a tracking theodolite or normal airfid radar. It is concluded that mean square throttle movement is a useful guide to the effect of speed stability on the difficulty of the approach, and corresponds with pilot ratings. Also, there are indications that throttle movements are unaffected by the type of talkdown control, whereas elevator, speed, and glide path measurements are altered appreciably. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1963
- Accession Number
- AD0426378
Entities
People
- K. J. Staples
Organizations
- AGARD