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Separable aircraft, control method and electronic equipment

An aircraft and separate technology, applied in the field of unmanned aerial vehicles, can solve the problems that fixed-wing unmanned aerial vehicles are difficult to meet the actual needs, unmanned aerial vehicles cannot meet the needs and other problems, and achieve the effect of widening the mission profile, reducing the impact, and quickly positioning.

Pending Publication Date: 2022-05-27
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the continuous advancement of science and technology, the application fields of drones have become more and more extensive in recent years, but as the application environment becomes more complex, traditional single-function drones will be difficult to meet actual needs
[0003] When it is necessary to fly in a complex environment, the traditional single-function fixed-wing UAV is obviously difficult to meet the actual needs

Method used

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  • Separable aircraft, control method and electronic equipment
  • Separable aircraft, control method and electronic equipment
  • Separable aircraft, control method and electronic equipment

Examples

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Embodiment 1

[0137] A detachable aircraft is formed by connecting a front aircraft and a rear aircraft, wherein the tail of the front aircraft is provided with a matching cabin that cooperates with the rear aircraft, the head of the rear aircraft is provided with a torsion-resistant positioning cabin, and the positioning cabin and the matching cabin are provided. Connected or separated by connecting structures.

[0138] The connection structure includes three positioning plates and degaussing electromagnets arranged on the positioning cabin, and iron sheets correspondingly arranged in the matching cabin. The three positioning plates are provided with hole structures corresponding to the size of the degaussing electromagnets, and the degaussing electromagnets are placed in the hole structures.

[0139] The front machine includes a first main wing and a second main wing symmetrically arranged on both sides of the front machine body, wherein the first main wing and the second main wing have a...

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PUM

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Abstract

The invention discloses a separable aircraft, a control method and electronic equipment. The separable aircraft is formed by connecting a front aircraft body and a rear aircraft body, the tail of the front aircraft body is provided with a matching cabin matched with the rear aircraft body, the head of the rear aircraft body is provided with an anti-torsion positioning cabin, and the positioning cabin and the matching cabin are connected or separated through a connecting structure. The separable aircraft can be separated into the front aircraft body and the rear aircraft body in the specified airspace, the front aircraft body and the rear aircraft body can independently complete operation, and the task load and the task execution efficiency of the aircraft can be improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a detachable aircraft, a control method and electronic equipment. Background technique [0002] With the continuous advancement of science and technology, the application fields of UAVs have become more and more extensive in recent years, but as the application environment becomes more complex, traditional single-purpose UAVs will be difficult to meet actual needs. [0003] When flying in complex environments is required, it is obviously difficult for traditional single-function fixed-wing UAVs to meet the actual needs. [0004] Therefore, it is urgent to design an aircraft that can change its shape during flight and combine the performance characteristics of different types of UAVs to improve the environmental adaptability, so as to better meet the mission requirements. SUMMARY OF THE INVENTION [0005] In view of the above problems in the prior art, the pres...

Claims

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Application Information

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IPC IPC(8): B64D5/00
CPCB64D5/00
Inventor 王佳楠张名洋宋士泽何晓宇罗野朱俊帆阮晨阳张艺弘姜浩舸王铮李欣波
Owner BEIJING INSTITUTE OF TECHNOLOGYGY