Flight Control of a Quadrotor Vehicle Subsequent to a Rotor Failure
Author:
Affiliation:
1. School of Electrical and Electronic Engineering, University of Manchester, Manchester, England M13 9PL, United Kingdom
2. Department of Information Engineering, Università Politecnica delle Marche, 60131 Ancona, Italy
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/10.2514/1.59869
Reference19 articles.
1. Dynamic inversion with zero-dynamics stabilisation for quadrotor control
2. Design of Robust Drag-Free Controllers with Given Structure
3. Kinematic Analysis and Control Design for a Nonplanar Multirotor Vehicle
4. Sliding-Mode Control Applied of a Nonlinear Model of an Unmanned Aerial Vehicle
5. CastilloP.LozanoR.DzulA. “Modelling and Control of Mini-Flying Machines,” 1st ed., Springer–Verlag, New York, 2005, pp. 39–59.
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