Application of Steep Angle Approach in an Engineering and Flight Test Program.
Abstract
This study is part of the Army program whose overall objectives are to determine the adequacy of the MLS guidance signals required for integration with state-of-the-art displays to enable safe, controlled, decelerating steep angle approaches and landings to be made by helicopters and to provide display hardware suitable for integration with the MLS Army prototype evaluation. The objective of this particular study is to apply the results of the previous JANAIR Steep Angle Approach and Landing study tasks, which have been analytic and simulation efforts, to a flight test of concepts, principles and mechanization.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1974
- Accession Number
- ADA005074
Entities
People
- James W. Wingert
Organizations
- Honeywell International, Inc.