Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds
Author:
Affiliation:
1. Davidson Technologies, Inc., Huntsville, Alabama 35806
2. University of Alabama in Huntsville, Huntsville, Alabama 35899
3. Z/I Imaging Corporation, Madison, Alabama 35757
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/10.2514/1.15486
Reference27 articles.
1. Nonlinear inverse dynamics control of aircraft using spoilers
2. Gain-scheduled missile autopilot design using linear parameter varying transformations
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