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Piloted simulation of an on-board trajectory optimization algorithmThis paper will describe a real time piloted simulation of algorithms designed for on-board computation of time-optimal intercept trajectories for an F-8 aircraft. The algorithms, which were derived using singular perturbation theory, generate commands that are displayed to the pilot on flight director needles on the 8-ball. By flying the airplane so as to zero the horizontal and vertical needles, the pilot flies an approximation to a time-optimal intercept trajectory. The various display and computation modes that are available will be described and results will be presented illustrating the performance of the algorithms with a pilot in the loop.
Document ID
19820036761
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Price, D. B.
(NASA Langley Research Center Hampton, VA, United States)
Calise, A. J.
(NASA Langley Research Center Hampton, VA, United States)
Moerder, D. D.
(Drexel University Philadelphia, PA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1981
Subject Category
Aircraft Communications And Navigation
Meeting Information
Meeting: Joint Automatic Control Conference, University of Virginia
Location: Charlottesville, VA
Start Date: June 17, 1981
End Date: June 19, 1981
Sponsors: AIChE, ASME, IEEE, and ISA,
Accession Number
82A20296
Distribution Limits
Public
Copyright
Other

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