Optimal Trajectory Shaping Guidance of Missiles with Time Varying Acceleration Constraints
52nd, Israel annual conference on aerospace sciences ; 2012 ; Tel-Aviv, Israel
2012-01-01
23 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Practical Stochastic Optimal Guidance Law for Bounded Acceleration Missiles
Online Contents | 2011
|Trajectory-Shaping Guidance for Interception of Ballistic Missiles During the Boost Phase
Online Contents | 2008
|