Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds
Authors:
- 1 May 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 29 (3) , 617-625
Abstract
No abstract availableKeywords
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