System and method for landing a mobile platform via a magnetic field

Abstract

A system for landing a mobile platform, such as an Unmanned Aerial Vehicle (“UAV”) and methods for making and using the same. The system can land the UAV by applying a magnetic levitation force upon the UAV and adjusting the applied magnetic levitation force. The system can initiate a landing process to a designated docking station and can guide the UAV to an adjacency of the designated docking station. Once the UAV has entered the adjacency, the magnetic levitation forces can take control of the landing process. During the landing process, certain magnetic sensitive devices installed on the UAV and/or on the designated docking station can be protected by turning them off or by shielding them. The system overcomes disadvantages of currently-available landing systems by restricting a size and weight of the landing arrangements, as well as, avoiding potential damage to the UAV and the designated docking station.

1 - 30 . (canceled) 
     
     
         31 . A landing system comprising:
 an unmanned aerial vehicle (UAV) configured to emit a first magnetic field;   a docking station configured to emit a second magnetic field opposing the first magnetic field, wherein the first magnetic field and the second magnetic field cooperatively generate a magnetic levitation force; and   one or more processors, individually or collectively, configured to:
 receive location information to determine whether the UAV is in an effective range of the docking station, wherein the location information includes one or more of global positioning system (GPS) data and visual positioning data; 
 in response to determining the UAV is in the effective range of the docking station, initiate an automatic landing process by controlling the magnetic levitation force to land the UAV onto the docking station; and 
 initiate a protective measure for protecting one or more magnetic sensitive devices of the UAV during the automatic landing process. 
   
     
     
         32 . The landing system of  claim 31 , wherein the one or more processors are disposed on the UAV, the docking station, or a remote device. 
     
     
         33 . The landing system of  claim 31 , wherein the first magnetic field is generated by a first magnetic arrangement disposed on the UAV and the second magnetic field is generated by a second magnetic arrangement disposed on the docking station, the first magnetic arrangement or the second magnetic arrangement comprising one or more of a permanent magnet and/or an adjustable magnet including an electromagnet. 
     
     
         34 . The landing system of  claim 31 , wherein the GPS data represents a location of the UAV and/or the docking station, and the visual positioning data represents a location of a visual sign at the docking station. 
     
     
         35 . The landing system of  claim 31 , wherein the effective range is formed by the second magnet field providing a half sphere boundary, a circular boundary, an elliptical boundary, or a rectangular boundary from the docking station. 
     
     
         36 . The landing system of  claim 31 , wherein the one or more processors are further configured to:
 control the magnetic levitation force by adjusting one or more of a frequency, a magnitude, a direction, and a distribution of the first magnetic field or the second magnetic field.   
     
     
         37 . The landing system of  claim 36 , wherein the one or more processors are further configured to:
 decrease or increase the frequency and/or the magnitude of the first magnetic field or the second magnetic field; or   change the direction and/or the distribution of the first magnetic field or the second magnetic field.   
     
     
         38 . The landing system of  claim 37 , wherein changing the direction and/or the distribution of the first magnetic field or the second magnetic field includes changing a magnetic pole of the first magnetic field or the second magnetic field. 
     
     
         39 . The landing system of  claim 31 , wherein the one or more magnetic sensitive devices comprise an image sensor including a high-definition image transferring sensor, or a position sensor including a GPS sensor or a compass. 
     
     
         40 . The landing system of  claim 31 , wherein the protective measure includes activating a first magnetic shield associated with the UAV or a second magnetic shield associated with the docking station to cover the one or more magnetic sensitive devices. 
     
     
         41 . The landing system of  claim 40 , wherein the first magnetic shield or the second magnetic shield comprises a metallic or magnetic material and is configured to attenuate the first magnetic field or the second magnetic field. 
     
     
         42 . The landing system of  claim 31 , wherein the protective measure includes deactivating the one or more magnetic sensitive devices, shutting down a power of the UAV, or shutting down a power of propellers of the UAV. 
     
     
         43 . A landing method comprising:
 receiving location information to determine whether an unmanned aerial vehicle (UAV) is in an effective range of a docking station, wherein the location information includes one or more of global positioning system (GPS) data and visual positioning data;   in response to determining the UAV is in the effective range of the docking station, initiate an automatic landing process by controlling a magnetic levitation force to land the UAV onto the docking station, wherein the magnetic levitation force is cooperatively generated by a first magnetic field that is emitted from the UAV and a second magnetic field opposing the first magnet field that is emitted from the docking station; and   initiating a protective measure for protecting one or more magnetic sensitive devices of the UAV during the automatic landing process.   
     
     
         44 . The landing method of  claim 43 , wherein the first magnetic field is generated by a first magnetic arrangement disposed on the UAV and the second magnetic field is generated by a second magnetic arrangement disposed on the docking station, the first magnetic arrangement or the second magnetic arrangement comprising one or more of a permanent magnet and/or an adjustable magnet including an electromagnet. 
     
     
         45 . The landing method of  claim 43 , wherein the GPS data represents a location of the UAV and/or the docking station, and the visual positioning data represents a location of a visual sign at the docking station. 
     
     
         46 . The landing method of  claim 43 , wherein the effective range is formed by the second magnet field providing a half sphere boundary, a circular boundary, an elliptical boundary, or a rectangular boundary from the docking station. 
     
     
         47 . The landing method of  claim 43 , further comprising:
 controlling the magnetic levitation force by adjusting one or more of a frequency, a magnitude, a direction, and a distribution of the first magnetic field or the second magnetic field.   
     
     
         48 . The landing method of  claim 47 , further comprising:
 decreasing or increasing the frequency and/or the magnitude of the first magnetic field or the second magnetic field; or   changing the direction and/or the distribution of the first magnetic field or the second magnetic field.   
     
     
         49 . The landing method of  claim 43 , wherein the protective measure includes activating a first magnetic shield associated with the UAV or a second magnetic shield associated with the docking station to cover the one or more magnetic sensitive devices. 
     
     
         50 . The landing method of  claim 43 , wherein the protective measure includes deactivating the one or more magnetic sensitive devices, shutting down a power of the UAV, or shutting down a power of propellers of the UAV