Optimal Feedback Guidance for Nonlinear Missile Model with Impact Time and Angle Constraints (AIAA 2013-4785)
Conference, Guidance, navigation and control; AIAA guidance ; 2013 ; Boston, MA
01.01.2013
12 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1937
British Library Conference Proceedings | 2015
|Optimal Control Framework for Impulsive Missile Interception Guidance (AIAA 2013-4787)
British Library Conference Proceedings | 2013
|Lead Angle Constrained Optimal Midcourse Guidance (AIAA 2013-4786)
British Library Conference Proceedings | 2013
|