US2021243258A1PendingUtilityA1

Aircraft and external device of the aircraft, communication method, device and system

Assignee: SZ DJI TECHNOLOGY CO LTDPriority: Mar 23, 2017Filed: Apr 8, 2021Published: Aug 5, 2021
Est. expiryMar 23, 2037(~10.6 yrs left)· nominal 20-yr term from priority
H04W 72/52B64U 2101/20B64U 2201/20H04B 1/0003H04L 67/34H04W 72/0453B64D 45/00H04L 67/12H04W 72/1268B64C 2201/122
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Claims

Abstract

A wireless communication method includes receiving, by an external device, a request to transmit data to an aircraft, in response to a triggering condition being satisfied, switching a communication electric circuit of the aircraft from operating a first software defined ration (SDR) firmware to operating a second SDR firmware, and receiving, by the aircraft, data to be transmitted. Communication electric circuits of the aircraft and the external device are respectively configured to execute corresponding SDR firmwares to establish communication links. The first SDR firmware is configured to establish a communication link of the aircraft, and the second SDR firmware is configured to establish a communication link of the external device. A bandwidth of a communication link of the aircraft operated with the second SDR firmware is broader than a bandwidth of the communication link of the aircraft operated with the first SDR firmware.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A wireless communication method, comprising:
 receiving, by an external device, a request to transmit data to an aircraft;   in response to a triggering condition being satisfied, switching a communication electric circuit of the aircraft from operating a first software defined ration (SDR) firmware to operating a second SDR firmware; and   receiving, by the aircraft, data to be transmitted, wherein:   communication electric circuits of the aircraft and the external device are respectively configured to execute corresponding SDR firmwares to establish communication links;   the first SDR firmware is configured to establish a communication link of the aircraft, and the second SDR firmware is configured to establish a communication link of the external device; and   a bandwidth of a communication link of the aircraft operated with the second SDR firmware is broader than a bandwidth of the communication link of the aircraft operated with the first SDR firmware.   
     
     
         2 . The wireless communication method of  claim 1 , further comprising:
 stopping loading a first SDR firmware into the communication electric circuit of the aircraft; and   loading a built-in second SDR firmware into the communication electric circuit of the aircraft.   
     
     
         3 . The wireless communication method of  claim 2 , further comprising:
 stopping loading the second SDR firmware into the communication electric circuit of the aircraft; and   loading the first SDR firmware into the communication electric circuit of the aircraft.   
     
     
         4 . The wireless communication method of  claim 1 , wherein:
 the triggering condition comprises a size of the data to be transmitted being greater than a predetermined data amount; and   after the aircraft completes receiving the data to be transmitted, the method further comprises:
 restoring the operation of the communication electric circuit of the aircraft to the first SDR firmware. 
   
     
     
         5 . The wireless communication method of  claim 1 , wherein the data to be transmitted comprise a firmware of the aircraft configured to upgrade the aircraft. 
     
     
         6 . The wireless communication method of  claim 2 , wherein the external device comprises a remote controller. 
     
     
         7 . A wireless communication method of  claim 1 , wherein:
 a communication link in the wireless communication system, through which the external device transmits data to the aircraft is an uplink; and   a communication link in the wireless communication system, through which the aircraft transmits data to the external device is a downlink.   
     
     
         8 . A wireless communication method of  claim 7 , wherein the triggering condition comprises a preset bandwidth of the uplink being narrower than a preset bandwidth of the downlink. 
     
     
         9 . A wireless communication method of  claim 8 , further comprising:
 in response to the preset bandwidth of the uplink being narrower than the preset bandwidth of the downlink, switching the communication link of the aircraft and the communication link of the external device, to increase the bandwidth of the uplink.   
     
     
         10 . An aircraft, comprising:
 a communication electric circuit configured to establish a communication link to wirelessly communicate with an external device;   a storage device configured to store a computer program;   a processor configured to execute the computer program to:
 obtain a data transmission request received through the communication electric circuit; 
 in response to a triggering condition being satisfied, based on the data transmission request, switching a communication electric circuit of the aircraft from operating a first software defined ration (SDR) firmware to operating a second SDR firmware; and 
 control the communication electric circuit to receive data to be transmitted through a communication link of the aircraft; and 
   an aircraft body configured to perform a flight based on flight instructions from the processor,   wherein:   communication electric circuits of the aircraft and the external device are respectively configured to execute corresponding SDR firmwares to establish communication links;   the first SDR firmware is configured to establish the communication link of the aircraft, and the second SDR firmware is configured to establish a communication link of the external device; and   a bandwidth of a communication link of the aircraft operated with the second SDR firmware is broader than a bandwidth of the communication link of the aircraft operated with the first SDR firmware.   
     
     
         11 . The aircraft of  claim 10 , wherein the processor is further configured to:
 stop loading a first SDR firmware into the communication electric circuit of the aircraft; and   load a second SDR firmware into the communication electric circuit of the aircraft.   
     
     
         12 . The aircraft of  claim 11 , wherein the processor is further configured to:
 stop loading the second SDR firmware into the communication electric circuit of the aircraft; and   load the first SDR firmware into the communication electric circuit of the aircraft.   
     
     
         13 . The aircraft of  claim 10 , wherein:
 the triggering condition comprises a size of the data to be transmitted being greater than a predetermined data amount; and   the processor is further configured to: after the aircraft completes receiving the data to be transmitted, restore the operation of communication electric circuit of the aircraft to the first SDR firmware.   
     
     
         14 . The aircraft of  claim 10 , wherein the data to be transmitted comprise a firmware of the aircraft configured to upgrade the aircraft. 
     
     
         15 . The aircraft of  claim 10 , further comprising:
 an acquisition device configured to transmit acquired data obtained through detection to the storage device,   wherein the processor is configured to retrieve the acquired data from the storage, and control the communication electric circuit to transmit the acquired data to the external device.   
     
     
         16 . The aircraft of  claim 11 , wherein the external device comprises a remote controller. 
     
     
         17 . The aircraft of  claim 10 , wherein:
 a communication link in the wireless communication system, through which the external device transmits data to the aircraft is an uplink; and   a communication link in the wireless communication system, through which the aircraft transmits data to the external device is a downlink.   
     
     
         18 . The aircraft of  claim 17 , the triggering condition comprises a preset bandwidth of the uplink being narrower than a preset bandwidth of the downlink. 
     
     
         19 . The aircraft of  claim 18 , wherein the processor is further configured to:
 in response to the preset bandwidth of the uplink being narrower than the preset bandwidth of the downlink, switch the communication link of the aircraft and the communication link of the external device, to increase the bandwidth of the uplink.

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