Unmanned aerial vehicle system having multi-rotor type rotary wing
The present invention relates to an unmanned aerial vehicle system having a multi-rotor type rotary wing. The unmanned aerial vehicle system having a multi-rotor type rotary wing includes a first unmanned aerial vehicle, at least one second unmanned aerial vehicle, and a bridge that connects the first unmanned aerial vehicle and the at least one second unmanned aerial vehicle to be separable from each other, wherein the at least one second unmanned aerial vehicle is moveable by the first unmanned aerial vehicle in a state where the at least one second unmanned aerial vehicle is coupled to the first unmanned aerial vehicle by the bridge without being driven, and the at least one second unmanned aerial vehicle is separable from the first unmanned aerial vehicle which is in flight.
1. An unmanned aerial vehicle system having a multi-rotor type rotary wing, comprising:
a first unmanned aerial vehicle;
a plurality of second unmanned aerial vehicles;
a bridge configured to connect the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles so that the plurality of second unmanned aerial vehicles are separable from the first unmanned aerial vehicle; and
a controller configured to, in response to one of the plurality of second unmanned aerial vehicles generating a first lift force for separating from the first unmanned aerial vehicle, reduce a second lift force being generated by the first unmanned aerial vehicle by an amount equal to the first lift force,
wherein the plurality of second unmanned aerial vehicles are moveable by the first unmanned aerial vehicle in a state in which the plurality of second unmanned aerial vehicles are coupled to the first unmanned aerial vehicle by the bridge without being driven, and
wherein the plurality of second unmanned aerial vehicles are configured to be coupled vertically above the first unmanned aerial vehicle by the bridge.
2. The unmanned aerial vehicle system of claim 1 , wherein the plurality of second unmanned aerial vehicles have a smaller size than a size of the first unmanned aerial vehicle.
3. The unmanned aerial vehicle system of claim 1 , wherein the controller is further configured to control the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles so that
in a state in which the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles are coupled to each other, the first unmanned aerial vehicle generates lift and the plurality of second unmanned aerial vehicles do not generate lift, and
in a state in which the one of the plurality of second unmanned aerial vehicles is separated from the first unmanned aerial vehicle, the first lift force remains constant, and the second lift force is set for the first unmanned aerial vehicle to hover.
4. The unmanned aerial vehicle system of claim 1 , wherein the controller is further configured to control the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles so that
the first unmanned aerial vehicle transports the plurality of second unmanned aerial vehicles up to a standby location, and
the plurality of second unmanned aerial vehicles separate from the first unmanned aerial vehicle at the standby location and enter a target location.
5. The unmanned aerial vehicle system of claim 4 , wherein the controller is further configured to set the standby location at an outdoor location, and set the target location at an indoor location.
6. The unmanned aerial vehicle system of claim 4 , wherein the controller is further configured to
control operations of the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles by wirelessly transmitting and receiving signals to and from the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles, and
control the plurality of second unmanned aerial vehicles that are entering the target location to transmit and receive signals to and from the controller through the first unmanned aerial vehicle that waits at the standby location.
7. The unmanned aerial vehicle system of claim 6 , further comprising:
a manipulator configured to manipulate the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles in real-time by wirelessly transmitting and receiving signals to and from the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles,
wherein the plurality of second unmanned aerial vehicles are configured to transmit an image obtained by photographing a surrounding space to the controller.
8. The unmanned aerial vehicle system of claim 6 , wherein the controller is further configured to control the plurality of second unmanned aerial vehicles to enter the target location to perform indoor location recognition, perform search operations, monitor an environment, monitor a temperature, and transmit a monitored result to the controller.
9. The unmanned aerial vehicle system of claim 1 , wherein
the bridge is further configured to electrically connect the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles, and
power is supplied from the first unmanned aerial vehicle to the plurality of second unmanned aerial vehicles through the bridge.
10. The unmanned aerial vehicle system of claim 1 , wherein the controller is further configured to, in response to determining that the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles reach a standby location, transmit a separation signal to the first unmanned aerial vehicle or the plurality of second unmanned aerial vehicles.
11. The unmanned aerial vehicle system of claim 1 , wherein the controller is further configured to, in response to the one of the plurality of second unmanned aerial vehicles detaching from the first unmanned aerial vehicle and thereby causing a change in a center of gravity of the first unmanned aerial vehicle and remaining attached vehicles among the second unmanned aerial vehicles, perform balancing control for the first unmanned aerial vehicle by predicting the change in the center of gravity.
12. An unmanned aerial vehicle system having a multi-rotor type rotary wing, comprising:
a first unmanned aerial vehicle;
a plurality of second unmanned aerial vehicles;
a bridge configured to connect the first unmanned aerial vehicle and the plurality of second unmanned aerial vehicles so that the plurality of second unmanned aerial vehicles are separable from the first unmanned aerial vehicle; and
a controller configured to, in response to one of the plurality of second unmanned aerial vehicles generating a first lift force for separating from the first unmanned aerial vehicle, reduce a second lift force being generated by the first unmanned aerial vehicle,
wherein the plurality of second unmanned aerial vehicles are moveable by the first unmanned aerial vehicle in a state in which the plurality of second unmanned aerial vehicles are coupled to the first unmanned aerial vehicle by the bridge without being driven,
wherein the plurality of second unmanned aerial vehicles are configured to be coupled vertically above the first unmanned aerial vehicle by the bridge, and
wherein the controller is further configured to, in response to the one of the plurality of second unmanned aerial vehicles detaching from the first unmanned aerial vehicle and thereby causing a change in a center of gravity of the first unmanned aerial vehicle and remaining attached vehicles among the second unmanned aerial vehicles, perform balancing control for the first unmanned aerial vehicle by predicting the change in the center of gravity.