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Flight array system with autonomous flight capability

An array and capability technology, applied in the field of flight array systems, can solve problems such as the inability to carry multiple loads to complete system functions, single-module UAVs occupying most of the space, and the flight system load capacity is limited, etc., to ensure autonomous flight capabilities. , The effect of flexible posture adjustment action, good mass production capacity

Active Publication Date: 2021-03-12
XIDIAN UNIV
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Problems solved by technology

[0006] In addition, the load capacity of the flight system designed in the above-mentioned scheme is limited. Most of the space of the single-module UAV is occupied by the power system. The limited load capacity cannot carry multiple loads to complete system functions, and it does not have the basic conditions for take-off in a small space.

Method used

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  • Flight array system with autonomous flight capability
  • Flight array system with autonomous flight capability
  • Flight array system with autonomous flight capability

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Embodiment Construction

[0033] The present invention will be described in detail below in conjunction with specific examples. The following description helps those skilled in the art to further understand the present invention, but does not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0034] Such as figure 1 As shown, a flight array system with autonomous flight capability: it is characterized in that: the single-module unmanned aerial vehicle of the flight array module at least includes: a full vector power unit 1, a body module 2, and a load module 3; the full vector power unit Unit 1 is used to provide the flight power and attitude adjustment power of the single-module UAV. The flight power is realized by the coaxial propeller, the attitude adjustment is realized by the parall...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a flight array system with autonomous flight capability. The system is characterized in that a single-module unmanned aerial vehicle of a flight array module at least comprises a full-vector power unit, a vehicle body module and a load module. The autonomous flight array module is small in occupied space, high in load capacity, flexible in posture adjustment and capable of taking off in a stacked mode in a narrow space.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a flight array system with autonomous flight capability. Background technique [0002] The development and application of UAVs have attracted great attention from various countries, and people have put forward higher requirements for the environmental adaptability and work fields of UAVs. The modular design of UAVs that perform complex functions, and the use of modular features to achieve some indicators that are difficult to meet in the overall design have gradually become the focus of research in various countries. Combining the modular design to realize the functional modularization of the overall system, and loading the functional load design into a single module, and then realizing the autonomous flight capability of a single load through structural design, to cope with the environment with limited take-off space, which will greatly enrich the fl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00B64C27/10B64C39/02B64D47/00
CPCB64C1/00B64C27/10B64C39/02B64D47/00B64U50/19B64U30/20B64U2201/10B64U10/10
Inventor 张树新姜伟涛王耀华段宝岩张硕代季鹏
Owner XIDIAN UNIV
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