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Flight control management system and method for multi-rotor unmanned aerial vehicle

A multi-rotor unmanned aerial vehicle, flight control technology, applied in the field of multi-rotor unmanned aerial vehicle flight control management system, can solve problems such as low efficiency and difficult operation, achieve reduced technical requirements, simple operation, and reduced flight range redundancy degree of effect

Pending Publication Date: 2020-07-24
NORTHEAST AGRICULTURAL UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to propose a flight control management system and method for multi-rotor UAVs in view of the problems of difficult operation and low efficiency when using UAVs for surveying and mapping in the prior art

Method used

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  • Flight control management system and method for multi-rotor unmanned aerial vehicle
  • Flight control management system and method for multi-rotor unmanned aerial vehicle
  • Flight control management system and method for multi-rotor unmanned aerial vehicle

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specific Embodiment approach 1

[0044] Specific implementation mode one: refer to figure 1 Describe this embodiment in detail, the flight control management system of a kind of multi-rotor unmanned aerial vehicle described in this embodiment, comprises: flight task setting module, flight task arrangement module, flight route setting module, communication module, flight safety inspection module, Real-time monitoring module, UAV flight control module and UAV flight status monitoring module;

[0045] The communication module includes a UAV communication module and a system communication module,

[0046] The flight task setting module is used to set the flight parameters of the multi-rotor UAV,

[0047] The flight task arrangement module is used to set the flight task area of ​​the multi-rotor UAV,

[0048] The flight route setting module is used to draw and display the flight trajectory of the multi-rotor UAV according to the flight parameters and the flight mission area of ​​the multi-rotor UAV,

[0049]The...

specific Embodiment approach 2

[0058] Specific implementation mode two: refer to figure 2 This embodiment is described in detail. This embodiment relates to a flight control management method of a multi-rotor unmanned aerial vehicle. The technical solution for realizing the present invention is as follows:

[0059] A flight control management method for a multi-rotor UAV, comprising the following steps:

[0060] Step 1, the flight parameter setting module of the present invention refers to setting flight altitude, lateral overlap and course overlap.

[0061] The flight mode setting module of the present invention refers to setting the unmanned flight mode of multi-rotor, including orthophoto, 360-degree panorama, plant protection mode, line patrol mode, etc., setting the UAV flight control management mode through the flight mode, It mainly affects flight trajectory planning and setting.

[0062] Step 2, the flight task arrangement module of the present invention refers to the delineation of the flight ta...

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Abstract

The invention provides a flight control management system and method for a multi-rotor unmanned aerial vehicle, and relates to the technical field of autonomous control of unmanned aerial vehicles. The problems that in the prior art, when an unmanned aerial vehicle is used for surveying and mapping, operation is difficult, and efficiency is low are solved. Most of unmanned aerial vehicle flight control software in the prior art needs to be manually operated by a pilot to take off and land, and can only automatically fly in a flight area according to a flight route. In other actual flight tasks, most of the unmanned aerial vehicle flight control software needs to be manually operated by the pilot to control the unmanned aerial vehicle in the whole process, including taking off, executing the tasks and landing, and controlling the unmanned aerial vehicle to complete the aerial photography task. Compared with the prior art, the flight control management system has the advantages of beingeasy to operate, convenient to carry, efficient, stable and high in autonomy, the unmanned aerial vehicle does not need to be manually controlled in the whole process, most flight accidents are effectively avoided, the technical requirements for industrial flight personnel are lowered, the accurate flight time and flight route are calculated in advance through autonomous flight control, the flightrange redundancy is reduced, the surveying and mapping efficiency is improved, and the project cost is saved.

Description

technical field [0001] The invention relates to the technical field of autonomous control of unmanned aerial vehicles, in particular to a flight control management system and method for multi-rotor unmanned aerial vehicles. Background technique [0002] The ground monitoring and control system of the UAV is the monitoring center and command control center of the UAV. flight data and control it. People have developed various ground stations according to different needs to help UAV flight controllers monitor and deal with UAVs accordingly, so as to ensure the safety of UAV flight and mission execution. As the center of command and control, the ground station monitors and controls flight data, flight parameters, flight process, aircraft trajectory, tasks performed, normal operation of communication links, and aircraft takeoff and landing. On the basis of completing basic tasks, it is required to be able to deal with various unknown emergencies and adapt to various environment...

Claims

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Application Information

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IPC IPC(8): G05D1/10G01C11/02B64F5/60
CPCB64F5/60G01C11/02G05D1/102
Inventor 姜芸王军杨继文
Owner NORTHEAST AGRICULTURAL UNIVERSITY
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