Integrated Higher-Order Sliding Mode Guidance and Autopilot for Dual Control Missiles
Author:
Affiliation:
1. University of Alabama in Huntsville, Huntsville, Alabama 35899
2. Davidson Technologies, Inc., Huntsville, Alabama 35805
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.36961
Reference23 articles.
1. Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds
2. Nonlinear Disturbance Observer-Enhanced Dynamic Inversion Control of Missiles
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