NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Automatic flight performance of a transport airplane on complex microwave landing system pathsDuring this demonstration the microwave landing system was utilized to provide the terminal configured vehicle B-737 airplane with guidance for automatic control on complex, curved descending paths with precision turns into short final approaches terminating in landing and roll-out, even when subjected to strong and gusty tail- and cross-wind components and severe wind shear. The data collected from more than fifty approach flights during the demonstration provided an opportunity to analyze airplane flight performance on a statistical basis rather than on a single flight record basis as is customarily done with limited data replication. Mean and standard deviation data are presented for approach flight path tracking parameters. In addition, the adverse wind conditions encountered during these flights are described using three-dimensional wind vector characteristics computed from the extensive on-board sensor data.
Document ID
19780018123
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walsh, T. M.
(NASA Langley Research Center Hampton, VA, United States)
Weener, E. F.
(Boeing Co. Seattle, United States)
Date Acquired
August 9, 2013
Publication Date
April 1, 1978
Publication Information
Publication: AGARD Guidance and Control Design Considerations for Low-Altitude and Terminal-Area Flight
Subject Category
Aircraft Communications And Navigation
Accession Number
78N26066
Distribution Limits
Public
Copyright
Other
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available