<tdalign="left"> This model represents a flight control system for a helicopter that controls pitch attitude, roll attitude and yaw rate based on pilot inputs from the cyclic and pedals. The flight control computer also closes the loop on three hydrualic actuators and has sensor inputs from three Attitude/Heading Reference Systems. </td>
<tdalign="left"> This model represents a flight control system for a helicopter that controls pitch attitude, roll attitude and yaw rate based on pilot inputs from the cyclic and pedals. The flight control computer also closes the loop on three hydrualic actuators and has sensor inputs from three Attitude/Heading Reference Systems. </td>