Control system for quad rotor UAV

Abstract

This paper presents the design, analysis and testing oj a control system Jor a quadrotor. The research is focused on the maneuverability oj the quadrotor hence the mechanical design was done together with the design of the controlling algorithm. Constraints which occur due to using pre-built quadrotors, were eliminated by using this methodology. This enables more aggressive and aerobatic flying compared to other systems designed with off-the-shelf quadrotors.