@inproceedings{803fbfc5af1c4fd18fd6dc4af7f1bd66,
title = "Dynamics and optimal control of quadrotor platform",
abstract = "This article is devoted to development of a mathematical model of quadrotor and its applications in the control system of such platform. It shows consecutive steps in developing the equations constituting the model. Various aerodynamic phenomena, such as Vortex Ring State or blade flapping are mentioned and taken into account. The assumptions and reasoning behind are discussed. The structure of a control system is presented. Justification of optimal LQ regulator is made. Simulation tests of control system performance are conducted. Simple way of creating flight trajectories is shown. The conclusions are stated about the level of insight necessary in the creation of a control-oriented and useable model of quadrotor platform.",
author = "Rados{\l}aw Zawiski and Marian B{\l}achuta",
year = "2012",
doi = "10.2514/6.2012-4915",
language = "English",
isbn = "9781600869389",
series = "AIAA Guidance, Navigation, and Control Conference 2012",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation, and Control Conference 2012",
note = "AIAA Guidance, Navigation, and Control Conference 2012 ; Conference date: 13-08-2012 Through 16-08-2012",
}