State Space System Modelling of a Quad Copter UAV
This provides a foundational modeling approach for controlling quad copter UAVs, which is incremental as it applies standard techniques to a specific domain.
The paper derived linear mathematical models for a quad copter UAV, developing 3DOF and 6DOF state-space models from Newtonian equations to address its inherent dynamic instability.
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.