Experimental Verification of Linear and Adaptive Control Techniques for a Two Degrees-of-Freedom Helicopter
Author:
Affiliation:
1. Mechanical and Aerospace Engineering, University of Texas at Arlington, Arlington, TX 76019 e-mail:
2. Associate Professor Mechanical and Aerospace Engineering, University of Texas at Arlington, Arlington, TX 76019 e-mail:
Abstract
Publisher
ASME International
Subject
Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering
Link
http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/doi/10.1115/1.4029273/6119097/ds_137_06_064501.pdf
Reference16 articles.
1. Castillo, P., Albertos, P., Garcia, P., and Lozano, R., 2006, “Simple Real-Time Attitude Stabilization of a Quad-Rotor Aircraft With Bounded Signals,” Proceedings of 45th IEEE Conference on Decision and Control, pp. 1533–1538.
2. Robust Attitude Regulation of a 3-DOF Helicopter Benchmark: Theory and Experiments;IEEE Trans. Ind. Electron.,2011
3. Robust LQR Attitude Control of a 3DOF Laboratory Helicopter for Aggressive Maneuvers;IEEE Trans. Ind. Electron.,2013
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