A flight control system to regulate an engine throttle and elevator of a model flight vehicle by an operator positioned external to and remote from the vehicle. A linkage mechanism positioned within the flight vehicle provides independent operation of the vehicles' elevator and throttle through a plurality of relatively rotational and linearly translatable levers. Elevator and throttle control cables connect the linkage mechanism to an outboard controller held by the operator. Independent movement of elevator and throttle control rods is achieved through rotation of the controller housing about a particular axis which activates one or both of the control members within the flight vehicle.
The model aircraft control for model aircraft comprises a handle housing, an elevator control group and a throttle control group, the elevator and throttle control groups being interconnected by means of linkages to balance differential forces applied to respective controls during operation of the aircraft.
A wired flying model airplane manipulation rack for manipulating the flying of a wired model airplane, including a swivel control mechanism having a U-frame turned about a metal axle horizontally through 360.degree. and a swivel member turned within the U-frame vertically over 180.degree., a traction mechanism adapted to change the direction of the applied force of the operator, for permitting the flying model airplane to be controlled to fly horizontally through 360.degree. and turned in different directions.
