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Unmanned aerial vehicle flight control system

A flight control system and unmanned aerial vehicle technology, applied in the field of unmanned aerial vehicles, can solve problems such as poor stability, complex structure, and complicated operation steps, and achieve the effects of good stability, precise control, and simple structure

Pending Publication Date: 2021-04-09
苏州流昴飞行器技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Among all kinds of unmanned aerial vehicles, the flight control system is its core component. At present, the reliability and stability of the flight control system need to be further improved, especially the flight control system of small unmanned aerial vehicles. Among them, the flight control system of most UAVs has poor stability, complex structure, and complicated operation steps, making it difficult to achieve fast and accurate control of UAVs.

Method used

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  • Unmanned aerial vehicle flight control system

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Embodiment Construction

[0015] The present invention will now be further described in detail in conjunction with the accompanying drawings and embodiments. These drawings are all simplified schematic diagrams, only illustrating the basic structure of the present invention in a schematic manner, so it only shows the composition related to the present invention.

[0016] Such as figure 1 As shown, a UAV flight control system includes a single-chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module, and a power supply module; the single-chip microcomputer and the data acquisition module and the wireless communication module And the power supply module is connected, the data collection module collects the data in the flight process of the drone, after the data collection, the data is fed back to the data analysis module, and the data analysis module is used to process and analyze the collected data, and obta...

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Abstract

The invention discloses an unmanned aerial vehicle flight control system which comprises a single chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module and a power supply module. The single chip microcomputer is connected with the data acquisition module, the wireless communication module and the power supply module, the data acquisition module acquires data in the flight process of the unmanned aerial vehicle and feeds back the data to the data analysis module after acquiring the data, and the data analysis module is used for processing and analyzing the acquired data to obtain the actual condition of an unmanned aerial vehicle in the flight process. The wireless communication module transmits processed data to the central processing module, the central processing module controls the flight action of the unmanned aerial vehicle, and the power supply module comprises a storage battery unit and a solar energy unit. Flight control over the unmanned aerial vehicle is achieved, the structure is simple, stability is good, and rapid and accurate control over the unmanned aerial vehicle can be achieved.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an unmanned aerial vehicle flight control system. Background technique [0002] With the improvement of social development and scientific and technological progress, the demand for the use of drones is increasing, such as the monitoring of forest pests in the forestry department, pesticide spraying, dynamic monitoring of forest fire prevention, and the surveying and mapping of land and landforms or emergencies in the land and resources department. Communications or disaster dynamic estimation and prevention in catastrophic geographical disaster areas, marine monitoring, etc., power wiring, line inspection, public security traffic management, urban management, and video shooting have also begun to be widely used. [0003] Among all kinds of unmanned aerial vehicles, the flight control system is its core component. At present, the reliability and stabil...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 黄俊
Owner 苏州流昴飞行器技术有限公司
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