Modeling and control of a quadrotor with variable geometry arms
The goal of this paper is to study the dynamics of a quadcopter using a variable geometry structure and discuss the advantages of using the geometry variation. A mathematical model has been described using simulation to show quadcopter dynamics. Based on the different geometric configurations of arms it is shown how the arms’ angles affect longitudinal and lateral dynamics. The design's assumptions refer to hovering and rotation with Euler angles. Simulation results show that both controllers stabilize the quadrotor and the amplitude of the vibrations is significantly decreased, compared to the vibration of a common quadcopter with fixed arms, by varying the arm's angle. The quadcopter remains stable and all Euler rotations are perfectly controlled.