Aircraft Maneuver Design Using Bifurcation Analysis and Sliding Mode Control Techniques
Author:
Affiliation:
1. Council of Scientific and Industrial Research–National Aerospace Laboratories, Bangalore 560 017, India
2. Indian Institute of Technology–Madras, Chennai 600 036, India
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/10.2514/1.56361
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