State Space System Modelling of a Quad Copter UAV
arXiv:1908.07401
Abstract
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.
This is the full version of our paper "State Space System Modelling of a Quad Copter UAV"