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NASA NTRS · Conference Paper

Description and flight performance of two systems for two-segment approach

Published 2019-07-12 From Legacy CDMS 3 authors

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

This paper describes two different avionic systems which were designed and developed to provide guidance and control for two-segment noise abatement approaches. The concept of a low-cost retrofit avionic system evolved into a special-purpose two-segment computer which required a DME collocated with the ILS glide-slope transmitter. This system was evaluated in a Boeing 727-200 aircraft. The second system is an area navigation (RNAV) system modified to include the two-segment approach. This system is more sophisticated than the first system and does not restrict usage to any specific navigation ground aid. The modified RNAV system is a Collins ANS-70A and is currently being evaluated in a DC-8-61 aircraft.

Authors

  • Wehrend, W. R.
  • Shigemoto, F. H.
  • Bourquin, K. R. NASA Ames Research Center

Citation: Wehrend, W. R., Shigemoto, F. H., Bourquin, K. R. (2019). Description and flight performance of two systems for two-segment approach. Legacy CDMS. NASA NTRS ID 19740058910. https://ntrs.nasa.gov/citations/19740058910 ↗