Design and Piloted Simulation of a Robust Integrated Flight and Propulsion Controller
Author:
Affiliation:
1. University of Leicester, Leicester, England LE1 7RH, United Kingdom
2. Defence and Evaluation Research Agency, Bedford, England MK41 6AE, United Kingdom
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/10.2514/2.4519
Reference16 articles.
1. Robust integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques
2. Robust Integrated Flight and Propulsion Controller for the Harrier Aircraft
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