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Flight control management computer power-down processing method and system for fixed-wing unmanned aerial vehicle

A technology for managing computers and unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve problems such as data loss, inability to continue monitoring and control, and inability to guarantee the safety of fixed-wing unmanned aerial vehicles, so as to achieve the effect of ensuring safety

Active Publication Date: 2021-11-23
XIAN LINGKONG ELECTRONICS TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] During the flight of the fixed-wing UAV, the flight control and management computer (also known as the flight control management computer) is an important device for state control, flight command sending and equipment command sending of the fixed-wing UAV. When the management computer loses power due to power failure, the fixed-wing UAV will lose control due to failure to receive instructions, and may even crash
[0004] In the current related technology, after the flight control management computer loses power and restores the power supply, it is necessary to restart the flight control related software to monitor and control the fixed-wing UAV again, but the data before the power failure has been lost. , cannot continue the monitoring and control before the power failure, and cannot guarantee the safety of fixed-wing UAVs

Method used

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  • Flight control management computer power-down processing method and system for fixed-wing unmanned aerial vehicle
  • Flight control management computer power-down processing method and system for fixed-wing unmanned aerial vehicle
  • Flight control management computer power-down processing method and system for fixed-wing unmanned aerial vehicle

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Embodiment Construction

[0065] For purposes of the present application, technical solutions and advantages clearer, the accompanying drawings and the following embodiments, the present application is further described in detail. It should be understood that the specific embodiments described herein are intended to explain the present application and is not intended to limit the present application.

[0066] Example embodiments disclosed flight control computer management system for fixed-wing UAV down process of the present application.

[0067] Refer figure 1 The system includes:

[0068] Obtaining module 101, configured to, when the control and management of flight through the wing UAV flight control computer management, real-time access data input and output management flight control computer;

[0069] Storing module 102, configured to save the output data to the input data memory for storing input and output data of the data memory is not lost when power down the flight control computer management;

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Abstract

The invention discloses a power-down processing method and system for a flight control management computer of a fixed-wing unmanned aerial vehicle. The method comprises the steps: obtaining the input and output data of the flight control management computer in real time when the flight control management computer carries out the flight control and management of the fixed-wing unmanned aerial vehicle; the input and output data are stored in a data memory, and the input and output data stored in the data memory cannot be lost when the flight control management computer is powered down; and when the flight control management computer restores power supply after power failure and in the starting process, the input and output data of the data memory are loaded to the flight control management computer. The method is used for monitoring and control before power failure after the fixed-wing unmanned aerial vehicle recovers after power failure, and the safety of the fixed-wing unmanned aerial vehicle is guaranteed.

Description

Technical field [0001] The present application relates to the field of unmanned aerial vehicles, particularly to a fixed-wing UAV flight control computer management processing method and system down. Background technique [0002] Fixed-wing UAV has a long battery life and high-flying, are widely used in border cruise, tactical reconnaissance, security monitoring, anti-terrorism, anti-smuggling, anti-narcotics, disaster monitoring, forest fire prevention, communications relay, weather monitoring and Geographic Information Survey and other practical applications. [0003] In the fixed-wing UAV flight, flight control and management computer (also referred to as the flight control computer management) is a fixed-wing UAV state control, important equipment and flight instruction apparatus transmits the transmission instruction, if the flight control due to manage computer power failure, when power failure occurs, it will result in fixed-wing UAV due to the loss of control can not rece...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F1/30B64C39/02
CPCG06F1/30B64C39/02
Inventor 侯利洋廖新涛王文龙刘宇郭宏选
Owner XIAN LINGKONG ELECTRONICS TECH CO LTD