The invention relates to a control bar for grip, traction and control of a traction unit which has the control means of the control device, steering, acceleration and possible elevation and descent integrated into the structure thereof, the control means able to be thumbwheels, push buttons, pressure sensors, a gyroscope, a joystick or any combination of the same, or electronic processing means that allow for voice recognition. It also has a control unit and another communications unit (either connected by wiring or wireless) as well as its own power supply integrated in the support structure or received from the traction unit.

Disclosed is a flying skateboard which comprises a bearing part, power parts, a main control module and altitude induction modules. The bearing part comprises a left foot bearing area and a right foot bearing area which are connected, can rotate oppositely when pedaled with foot soles of a human body and can be located on the same plane or on different planes. The main control module comprises a gyroscope and used for controlling the power output of the power parts to keep the balance of the flying skateboard and make the flying skateboard to vertically move up and down or hover. The altitude induction modules are used for measuring the distances between the altitude induction modules and the ground to make the flying altitude of the flying skateboard within the altitude limit threshold value range.

Disclosed is a flying skateboard which comprises a bearing part, power parts, a main control module and altitude induction modules. The bearing part comprises a left foot bearing area and a right foot bearing area which are connected, can rotate oppositely when pedaled with foot soles of a human body and can be located on the same plane or on different planes. The main control module comprises a gyroscope and used for controlling the power output of the power parts to keep the balance of the flying skateboard and make the flying skateboard to vertically move up and down or hover. The altitude induction modules are used for measuring the distances between the altitude induction modules and the ground to make the flying altitude of the flying skateboard within the altitude limit threshold value range.

A transportation tool is configured to carry a rider. A sensor detects weight shifts of the rider on the body of the transportation tool. A controller, based on information from the sensor, generates control signals for an unmanned aerial vehicle. A communication device communicates the control signals to the unmanned aerial vehicle. A cable attaches to the aerial vehicle and to the rider or the body of the transportation tool.

The present application aims to provide an aircraft control method and an aircraft system, which can simplify the control of an aircraft combination having a pedal moving device arranged at the foot, so that it is easier for a person to carry the aircraft to walk, take off and land, the aircraft is easy to control, and the coordination problem of portions is solved. The aircraft control method comprises the following steps: an aircraft is fixedly connected to a person, and is supported by the feet of the person on the ground; a pedal moving device is provided for the feet of the person, and can carry the person and the aircraft to move on the ground; an operation-state information transmission device is provided between the aircraft and the pedal moving device; and the control of the pedal moving device is associated with the control of the aircraft by means of the information transmission device. The aircraft system, comprising an aircraft body and a pedal moving device, wherein the aircraft body is fixedly connected to a person, and is supported by the feet of the person on the ground, and the pedal moving device is provided for the feet of the person.