Study of a Half Small Scale Quadricopter Balance: Illustration of a Complex Analogue Electronic Feed Back
Author:
Affiliation:
1. Université de Bordeaux IPB UMR 5818, Av Dr. A. Schweitzer 33405 Talence, FRANCE
2. Université de Bordeaux, IUT GEII, 15 rue Naudet 33175 Gradignan, FRANCE
Abstract
Publisher
World Scientific and Engineering Academy and Society (WSEAS)
Subject
Electrical and Electronic Engineering
Reference20 articles.
1. Parrot frenchcompany web site:https://www.parrot.com/fr/drones/anafi
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3. N. Koksal, H. An and B. Fidan, “Two-Level Nonlinear Tracking Control of a Quadrotor Unmanned Aerial Vehicle” in Proc. IFAC-PapersOnLine, vol. 49, no. 17, pp. 254-259, 2016.
4. C. Izaguirre-Espinosa, A.J. Munoz-Vazquez, A. Sanchez-Orta, V. Parra-Vega and P. Castillo, “Attitude control of quadrotors based on fractional sliding modes: theory and experiments” IET Control Theory Applications, vol. 10, no. 7, pp. 825-832, 2016.
5. M. Hedayatpour, M. Mehrandezh and F. Janabi-Sharifi, “A unified approach to configuration based dynamic analysis of quadcopters for optimal stability” Int. Conference on Intelligent Robots and Systems (IROS), pp. 5116-5121, Vancouver, BC, Canada, September 2017.
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