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Differential game theory with applic...
~
Faruqi, Farhan A., (1944-)
Differential game theory with applications to missiles andautonomous systems guidance /
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Differential game theory with applications to missiles andautonomous systems guidance // Farhan A. Faruqi
Author:
Faruqi, Farhan A.,
Published:
Hoboken, NJ :John Wiley & Sons, : 2017.,
Description:
xv, 193 p. :ill. ; : 26 cm.;
Subject:
Guided missiles - Guidance systems -
ISBN:
1119168473 (cloth) :
Differential game theory with applications to missiles andautonomous systems guidance /
Faruqi, Farhan A.,1944-
Differential game theory with applications to missiles andautonomous systems guidance /
Farhan A. Faruqi - Hoboken, NJ :John Wiley & Sons,2017. - xv, 193 p. :ill. ;26 cm. - Aerospace series . - Aerospace series (Chichester, England) .
Includes bibliographical references and index
Differential game theory and applications to missile guidance -- Optimum control and differential game theory -- Differential game theory applied to two-party missile guidance problem -- Three-party differential game theory applied to missile guidance problem -- Four degrees-of-freedom (DOF) simulation model for missile guidance and control systems -- Three-party differential game missile guidance simulation study
ISBN: 1119168473 (cloth) :NT4507
LCCN: 2017000484 Subjects--Topical Terms:
1129613
Guided missiles
--Guidance systems
LC Class. No.: UG1310 / F251 2017
Dewey Class. No.: 623.4/519
Differential game theory with applications to missiles andautonomous systems guidance /
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1944-
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Differential game theory with applications to missiles andautonomous systems guidance /
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Farhan A. Faruqi
260
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Hoboken, NJ :
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John Wiley & Sons,
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2017.
300
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xv, 193 p. :
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ill. ;
$c
26 cm.
490
1
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Aerospace series
504
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Includes bibliographical references and index
505
0
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Differential game theory and applications to missile guidance -- Optimum control and differential game theory -- Differential game theory applied to two-party missile guidance problem -- Three-party differential game theory applied to missile guidance problem -- Four degrees-of-freedom (DOF) simulation model for missile guidance and control systems -- Three-party differential game missile guidance simulation study
650
0
$a
Guided missiles
$x
Guidance systems
$x
Mathematical models
$3
1129613
650
0
$a
Guided missiles
$x
Control systems
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Mathematical models
$3
1129612
650
0
$a
Game theory
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1129611
650
0
$a
Differential games
$3
1129610
830
0
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Aerospace series (Chichester, England)
$3
839674
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E044447
圖書館3F 書庫
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623.4519 F247 2017
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