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.