Nonlinear Autopilot Design for an Asymmetric Missile Using Robust Backstepping Control
Author:
Affiliation:
1. Department of Computer, Control and Management Engineering “Antonio Ruberti,”, University of Rome “La Sapienza,” 00185 Rome, Italy
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.G000434
Reference28 articles.
1. Combined Optimal/Classical Approach to Robust Missile Autopilot Design
2. GazzinaA. “How to Control Unstable Missile Airframes: Methodology and Limitations,” TR, Rome, 1989.
3. Gain-scheduled missile autopilot design using linear parameter varying transformations
4. Gain scheduling for H-infinity controllers: a flight control example
5. Dynamic scheduling of modern-robust-control autopilot designs for missiles
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