Computational method for determining the no-escape envelope of a short- range missile
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1990-01, Vol.13, p.3493-3493 |
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container_title | Journal of guidance, control, and dynamics |
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creator | Neuman, Frank |
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identifier | ISSN: 0731-5090 |
ispartof | Journal of guidance, control, and dynamics, 1990-01, Vol.13, p.3493-3493 |
issn | 0731-5090 |
language | eng |
recordid | cdi_proquest_miscellaneous_25599533 |
source | Alma/SFX Local Collection |
title | Computational method for determining the no-escape envelope of a short- range missile |
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