State Space System Modelling of a Quad Copter UAV
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Abstract (arXiv)
In this paper, a linear mathematical model for a quad copter unmanned aerial vehicle (UAV) is derived. The three degrees of freedom (3DOF) and six degrees of freedom (6DOF) quad copter state-space models are developed starting from basic Newtonian equations. These state space models are very important to control the quad copter system which is inherently dynamically unstable.
Key facts. Cited by 1 paper in the map (data through 14 Oct 2026). First posted on arXiv 20 Aug 2019.
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