Flight fault emergency processing method and system

A technology for emergency treatment and failure, applied in control/regulation systems, aircraft component testing, non-electric variable control, etc., can solve problems such as high risk, hidden dangers of personal safety and property safety of ground personnel, and single processing mechanism to achieve flight safety Reliable and guarantee the effect of personal and property safety

Pending Publication Date: 2021-02-19
GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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Problems solved by technology

[0002] During the flight of drones in the air, internal factors or external environmental factors may cause unexpected situations such as failure of airborne electronic equipment or interruption of information. The occurrence of this situation has brought hidden dangers to the personal safety and property safety of ground personnel, especially The risk is greater when the UAV is outside the line of sight of the ground monitoring personnel. When dealing with this situation, most UAVs often adopt a relatively simple processing mechanism, such as returning to the voyage or opening an umbrella to land, etc., to ensure the flight of the UAV. Safe, but this processing method does not take measures for the possibility of fault recovery, which reduces the cost-effectiveness of drones

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  • Flight fault emergency processing method and system
  • Flight fault emergency processing method and system
  • Flight fault emergency processing method and system

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Embodiment Construction

[0029] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Apparently, the described embodiments are some, but not all, embodiments of the present invention. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0030] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative...

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Abstract

The invention discloses a flight fault emergency processing method and system, and relates to the field of flight fault processing. The method comprises the steps: S1, monitoring and collecting flightstate parameters in real time; S2, analyzing the flight state parameters to confirm flight fault conditions; S3, judging the priority of the flight fault condition, forming an execution strategy, andissuing the execution strategy to an unmanned aerial vehicle; and S4, controlling flight according to the execution strategy. The device comprises a data acquisition module, a data analysis module, afault strategy module and a flight control module. According to the invention, priority ranking is carried out on all the fault types, and an execution strategy is formed to control flight of an unmanned aerial vehicle, so that the application value of single flight of the unmanned aerial vehicle is maximized; measures corresponding to all the fault types are refined, and judgment processing of fault recovery is added, so that flight safety of the unmanned aerial vehicle is more reliable, and personal and property safety can be better guaranteed; and a fault priority discrimination module isadditionally arranged to sort various fault types of the unmanned aerial vehicle and generate a corresponding execution strategy, so that the single flight application value of the unmanned aerial vehicle is maximized.

Description

technical field [0001] The invention relates to the field of flight fault processing, in particular to an emergency processing method and system for flight faults. Background technique [0002] During the flight of drones in the air, internal factors or external environmental factors may cause unexpected situations such as failure of airborne electronic equipment or interruption of information. The occurrence of this situation has brought hidden dangers to the personal safety and property safety of ground personnel, especially The risk is greater when the UAV is outside the line of sight of the ground monitoring personnel. When dealing with this situation, most UAVs often adopt a relatively simple processing mechanism, such as returning to the voyage or opening an umbrella to land, etc., to ensure the flight of the UAV. It is safe, but this processing method does not take measures for the possibility of fault recovery, which reduces the cost-effectiveness of drones. Conten...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10B64F5/60
CPCG05D1/101B64F5/60
Inventor 邓坤赵林东陈强洪袁鸣鲍泳林李皓周欢
Owner GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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