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Studies of aircraft differential maneuvering. Report 75-27: Calculating of differential-turning barrier surfaces. Report 75-26: A user's guide to the aircraft energy-turn and tandem-motion computer programs. Report 75-7: A user's guide to the aircraft energy-turn hodograph programThe numerical analysis of composite differential-turn trajectory pairs was studied for 'fast-evader' and 'neutral-evader' attitude dynamics idealization for attack aircraft. Transversality and generalized corner conditions are examined and the joining of trajectory segments discussed. A criterion is given for the screening of 'tandem-motion' trajectory segments. Main focus is upon the computation of barrier surfaces. Fortunately, from a computational viewpoint, the trajectory pairs defining these surfaces need not be calculated completely, the final subarc of multiple-subarc pairs not being required. Some calculations for pairs of example aircraft are presented. A computer program used to perform the calculations is included.
Document ID
19760014100
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kelley, H. J.
(Analytical Mechanics Associates, Inc. Jericho, NY, United States)
Lefton, L.
(Analytical Mechanics Associates, Inc. Jericho, NY, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-137819
REPT-75-27
Report Number: NASA-CR-137819
Report Number: REPT-75-27
Accession Number
76N21188
Funding Number(s)
CONTRACT_GRANT: NAS2-8738
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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