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Computing The No-Escape Envelope Of A Short-Range MissileMethod for computing no-escape envelope of short-range air-to-air missile devised. Useful for analysis of both strategies for avoidance and strategies for attack. With modifications, also useful in analysis of control strategies for one-on-one air-to-air combat, or wherever multiple control strategies considered.
Document ID
19910000335
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Neuman, Frank (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
July 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12404
Accession Number
91B10335
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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