Control system for quadrotor uav

Abstract

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