Driving method and system of four-rotor-wing unmanned flight vehicle

A technology of unmanned aerial vehicles and driving methods, which is applied in the field of driving methods and systems of quadrotor unmanned aerial vehicles, can solve problems such as driving problems of quadrotor unmanned aerial vehicles, and achieve low maintenance costs, high system stability, and high reliability and safety effects

Inactive Publication Date: 2012-07-18
FOSHAN AIRCAM UAV TECH CORP
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Problems solved by technology

[0003] The purpose of the present invention is to provide a driving method of a quadrotor unmanned aerial vehicle, which is used to solve the driving problem of a quadrotor unmanned aerial vehicle
[0004] Another object of the present invention is to provide a driving system for a quadrotor unmanned aerial vehicle, which is used to solve the driving problem of a quadrotor unmanned aerial vehicle

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  • Driving method and system of four-rotor-wing unmanned flight vehicle
  • Driving method and system of four-rotor-wing unmanned flight vehicle
  • Driving method and system of four-rotor-wing unmanned flight vehicle

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[0040] The preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described below are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0041] figure 1 Shows the schematic flow chart of the driving method of the quadrotor unmanned aerial vehicle provided by the present invention, as figure 1 Shown:

[0042] In step S101, the ground station plans navigation information according to the terrain map, and transmits the navigation information to the onboard automatic driving control unit.

[0043] Before the aircraft starts, after the ground station extracts the target map from the topographic map, the flight path of the aircraft is determined on the target map, and then multiple waypoints are determined on the flight path. Determine the latitude and longitude coordinates, altitude, directio...

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Abstract

The invention discloses a driving method and a system of a four-rotor-wing unmanned flight vehicle. The method comprises the following steps that: navigation information is planned by a ground station according to a topographic map, and the navigation information is transmitted to a machine-mounted automatic driving control unit; after the flight vehicle is started, a sensing data automatic analysis processing unit generates current flight vehicle data according to current status information of the flight vehicle and transmits the current flight vehicle data to the machine-mounted automatic driving control unit; and the machine-mounted automatic driving control unit controls the flight vehicle to fly according to the navigation information and the current flight vehicle data. A flight path of the unmanned flight vehicle is planned on a target map, a plurality of discontinuous flight points are planned on the flight path, so the driving problem of the four-rotor-wing unmanned flight vehicle can be solved, advantages such as high reliability and high safety can guarantee the completion of different tasks, and advantages such as high hardware integration degree, high flexibility, high system stability, low maintenance cost and the like can be realized.

Description

technical field [0001] The invention relates to the driving of an aircraft based on a quadrotor structure, in particular to a driving method and system for a quadrotor unmanned aerial vehicle. Background technique [0002] At present, UAV (Unmanned Aerial Vehicles, referred to as UAV) is widely used in many fields such as aerial remote sensing, land surveillance, urban planning, water conservancy construction, forestry management, real-time monitoring, aerial reconnaissance, film and television aerial photography, advertising photography and military affairs. Due to the advantages of UAVs such as small size and light weight, they have been widely promoted, but the requirements of safety, stability, high cost performance and strong adaptability to the environment have not yet been realized, which puts forward high requirements for UAVs. With the increasingly higher requirements for intelligent design, the requirement for fully automatic and intelligent execution of tasks has ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C13/18G08G5/06
Inventor 安康
Owner FOSHAN AIRCAM UAV TECH CORP
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