This article is presenting the extended model of quadrotor platform together with a bespoken control system based on optimal approach. It highlights particular aspects of the derived model, such as inclusion of rotor gyroscopic effects and thrust generation based on momentum theory. The controller’s behavior is tested by simulations. Comparisons with literature-available solutions to the problem of full quadrotor optimal control are made and important differences exposed. Conclusions are drawn and future work proposed.
Chosen aspects of modeling and control of quadrotor platform
9TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES: ICNPAA 2012 ; 2012 ; Vienna, Austria
AIP Conference Proceedings ; 1493 , 1 ; 1116-1123
2012-11-06
8 pages
Conference paper
Electronic Resource
English
Chosen aspects of modeling and control of quadrotor platform
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