Nonlinear Control of Hypersonic Missiles for Maximum Target Penetration
Author:
Affiliation:
1. University of Florida
2. Embry-Riddle Aeronautical University
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4886
Reference26 articles.
1. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle
2. Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects
3. Control of a Flexible, Hypersonic Scramjet Vehicle Using a Differential Algebraic Approach
4. LPV Control Design for Over-Actuated Hypersonic Vehicles Models
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1. Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile;International Journal of Adaptive Control and Signal Processing;2016-01-20
2. Acceleration-free Nonlinear Guidance and Tracking Control of Hypersonic Missiles for Maximum Target Penetration;AIAA Guidance, Navigation, and Control Conference;2016-01-01
3. Adaptive Continuous Higher Order Sliding Mode Control of Air Breathing Hypersonic Missile for Maximum Target Penetration;AIAA Guidance, Navigation, and Control Conference;2015-01-02
4. Preliminary Aero-thermal Structural Simulation;14th AIAA Aviation Technology, Integration, and Operations Conference;2014-06-13
5. Robust Image-based Visual Servo Control of an Uncertain Missile Airframe;IFAC Proceedings Volumes;2014
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