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Theory for computing the size and shape of a region of influence associated with a maneuvering vehicleA general procedure for computing the region of influence of a maneuvering vehicle is described. Basic differential geometric relations, including the use of a general trajectory parameter and the introduction of auxiliary variables in the envelope theory are presented. To illustrate the application of the method, the destruct region for a maneuvering fighter firing missiles is computed.
Document ID
19800015769
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Barger, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1648
L-13419
Accession Number
80N24261
Funding Number(s)
PROJECT: RTOP 505-43-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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