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Unmanned aerial vehicle control system

A control system and drone technology, applied in the field of drones, can solve the problems of drones losing contact, drone crashes, etc., and achieve the effects of increasing communication reliability, low cost, and strong practicability

Inactive Publication Date: 2018-12-07
HEFEI CAREER TECHNICAL COLLEGE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the UAV has communication failures such as signal interruption many times during the flight in the air, the manifestation will be that the UAV loses contact instantaneously. Such a failure has a major safety hazard of the UAV crashing due to loss of control.

Method used

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Embodiment Construction

[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0028] The overall structure of unmanned aerial vehicles includes fuselage, airborne electronic equipment (navigation and attitude control, etc.), and take-off and landing assistance systems, etc. UAVs have no less requirements for aircraft than small unmanned reconnaissance aircraft. First of all, s...

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Abstract

The invention discloses an unmanned aerial vehicle control system. The unmanned aerial vehicle control system is composed of a flight control device and a user control terminal, the user control terminal receives an operation control instruction from a user and transmits the operation control instruction to the flight control device, the flight control device receives the operation control instruction from the user control terminal and controls an unmanned aerial vehicle according to the instruction, and the flight control device and the user control terminal perform data interaction through awireless link. The whole system runs stably, all modules of the system meet the design requirements, and the unmanned aerial vehicle control system has the characteristics of low cost, small volume,light weight, high reliability, easy operation, high practicability, etc.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle control system. Background technique [0002] Due to its low cost, small size, light weight, strong maneuverability, and long battery life, small UAVs are more and more widely used in the civilian field. The control of traditional civilian small drones is mainly completed by single-chip microcomputers. Its main disadvantages are insufficient data processing capabilities and poor real-time performance. Usually, it can only complete a single or relatively simple task. The rapid development of microelectronics technology has expanded the application field of UAVs. In recent years, UAVs have been more and more widely used in agriculture, meteorology, disaster monitoring and military affairs. The application of new technologies has improved the navigation performance of UAVs, but the navigation and control of the above-mentioned small UAVs ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/707H04L12/703H04W4/40H04L29/08G05D1/10H04L45/24H04L45/28
CPCH04L45/22H04L45/28H04L67/12H04W4/40G05D1/101H04L67/52
Inventor 盛凯吕菲张平华范士领丁小一宋聪颖邹子辉
Owner HEFEI CAREER TECHNICAL COLLEGE
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