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UAV (Unmanned Aerial Vehicle) endurance system

A technology of unmanned aerial vehicles and monitoring systems, applied in the field of unmanned aerial vehicles, can solve problems such as limited battery life, and achieve the effect of solving limited battery life and fast and accurate positioning

Inactive Publication Date: 2019-04-02
NANJING KAITIANYAN UAV TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the rapid development of the UAV industry, UAVs are increasingly widely used in people's production and life. However, due to the bottleneck in the development of the battery industry, the battery life of UAVs when performing flight tasks continuously and dynamically in a large range very limited capacity

Method used

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  • UAV (Unmanned Aerial Vehicle) endurance system

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Embodiment Construction

[0016] In order to describe the technical content, achieved goals and effects of the present invention in detail, the following descriptions will be made in conjunction with the embodiments and accompanying drawings.

[0017] Such as figure 1 As shown, the system includes a drone and a monitoring vehicle, and the monitoring vehicle is wirelessly connected to the drone; the drone includes a GPS module, an IMU inertial measurement module, a flight attitude controller, and a main control processor MCU; The GPS module and the IMU inertial measurement module are all electrically connected to the main control processor MCU, the main control processor MCU is electrically connected to the flight attitude controller, and the flight attitude controller is electrically connected to the motor; the monitoring vehicle includes an unmanned Aircraft monitoring system, power detection module and automatic charging device; the GPS module and IMU inertial measurement module perceive the position...

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Abstract

The invention provides a UAV endurance system, which comprises a UAV and a monitoring vehicle. The monitoring vehicle is wirelessly connected to the UAV. The UAV comprises a GPS module, an IMU inertiameasuring module, a flight attitude controller, a main control unit MCU. The GPS module and the IMU inertia measuring module are electrically connected to the main control unit MCU. The main controlunit MCU is electrically connected to the flight attitude controller which is electrically connected to a motor. The monitoring vehicle comprises a UAV monitoring system, a power quantity detecting module, and an automatic charger. The monitoring vehicle monitors information such as positions, flight attitudes, and power quantity of the UAV in real time by the UAV monitoring system. The UAV monitoring system controls the UAV to land on the monitoring vehicle and charges the UAV by the automatic charger. The UAV endurance system solves a problem that the endurance capability of the UAV is limited, and ensures that the UAV continuously and dynamically performs flight tasks in a large range.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle endurance system. Background technique [0002] With the rapid development of the UAV industry, UAVs are increasingly widely used in people's production and life. However, due to the bottleneck in the development of the battery industry, the battery life of UAVs when performing flight tasks continuously and dynamically in a large range Capabilities are very limited. Generally, the flight time of the UAV system for civilian use is more than 20 minutes, and the flight time of the UAV system used in the industry is only 1-2 hours. [0003] Using the combination of GPS and inertial navigation, the drone can be positioned quickly and accurately in complex environments. Through the path planning of the drone, the drone can accurately follow its own remaining power and current position under certain constraints. Fly to the designated locatio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10H02J7/00
CPCG05D1/0808G05D1/101H02J7/025H02J50/00
Inventor 陈冲张彪丘仲锋曹政石晓雨
Owner NANJING KAITIANYAN UAV TECH CO LTD
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