Guidance and Autopilot for Missiles Steered by Aerodynamic Lift and Divert Thrusters Using Second Order Sliding Mode Control
Author:
Affiliation:
1. University of Alabama in Huntsville
2. Davidson Technologies
3. Z/I Imaging Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6784
Reference32 articles.
1. 1P.Garnell,andD.J.East,GuidedWeaponControlSystems,Oxford:PergamonPress,1977.
2. Robust guidance for electro-optical missiles
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