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Optimum horizontal guidance techniques for aircraftSome problems of automatic guidance of an aircraft in the horizontal plane are described. The horizontal guidance tasks, which such a flight control system should be capable of performing, were identified as being of three types: guiding the aircraft from any initial location and initial heading to (1) any final location and heading; (2) intercept and fly along a line of specified direction; and (3) a final location with arbitrary final heading. Guidance problems such as capturing an ILS beam at a specified point on the beam, intercepting a VOR radial, and point-to-point navigation can be formulated in terms of these problems. The guidance laws minimize the arc distance to fly between initial and final conditions subject to constraints on the minimum turning radius.
Document ID
19780015073
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Erzberger, H.
(NASA Ames Research Center Moffett Field, CA, United States)
Lee, H. Q.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA, Washington Fourth Inter-Center Control Systems Conf.
Subject Category
Aircraft Communications And Navigation
Accession Number
78N23016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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