Integrated Autopilot and Guidance Design for Dual Controlled Missiles with Terminal Intercept Angle Constraint
53rd, Israel annual conference on aerospace sciences ; 2013 ; Tel-Aviv, Israel
2013-01-01
21 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Integrated Sliding Mode Autopilot-Guidance for Dual-Control Missiles
Online Contents | 2007
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