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
01.01.2013
21 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Integrated Sliding Mode Autopilot-Guidance for Dual-Control Missiles
Online Contents | 2007
|