Modeling of quadrotor helicopter dynamics

Quadrotor Helicopter or simply quadrotor is rotorcraft that has four lift-generating propellers. Two of the propellers spin clock wise and the other two counter-clockwise. Control of the machine can be achieved by varying relative speed of the propellers. Quadrotor concept is not new, however the modem quadrotors are mostly unmanned. Advancement in miniaturized MW technology, availability of high speed brushless motors and high power to weight ratio Li-Polymer battery technology, quadrotors can now be successfully designed and fabricated. This paper proposes a mathematical model of quadrotor dynamics. A simplified approach is adopted using momentum theory, where the gyroscopic effect and air friction on frame of machine has been neglected, resulting in a simplified model, which is useful for designing a controller to stabilize the machine in hover state. Proposed model is non-linear since the rotor dynamics are a function of square of motor inputs.