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An automatic launch and recovery device and method based on an unmanned vehicle

A technology of automatic launch and recovery device, applied in the direction of launch / tow transmission device, ground device, stop device, etc., can solve the problem of limiting the use scene and application scope of UAV system, economy, ease of use, safety, reliability It is difficult to achieve a balance between durability automation and intelligence, and achieve the effect of broadening product application scenarios, improving flight aerodynamic efficiency, and simplifying structure

Active Publication Date: 2022-05-24
AEROSPACE TIMES FEIHONG TECH CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These existing launch and recovery methods, for small and medium-sized fixed-wing UAV systems, are difficult to achieve a balance in terms of economy, ease of use, safety, reliability and durability, automation and intelligence, and are limited to a certain extent. UAV system usage scenarios and application scope
[0003] At the same time, the existing patents are for the unmanned transport platform to be equipped with a replaceable launch and recovery module, or the design of the unmanned vehicle rotary-wing unmanned aerial vehicle release and recovery platform. The coordinated launch and recovery of fixed-wing and unmanned vehicles are in the foreground at home and abroad. R & D stage

Method used

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  • An automatic launch and recovery device and method based on an unmanned vehicle
  • An automatic launch and recovery device and method based on an unmanned vehicle
  • An automatic launch and recovery device and method based on an unmanned vehicle

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Embodiment Construction

[0055]In order to better understand the technical solutions of the present invention, the embodiments of the present invention are described in detail below with reference to the accompanying drawings.

[0056] It should be understood that the described embodiments are only some, but not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0057] The terms used in the embodiments of the present invention are only for the purpose of describing specific embodiments, and are not intended to limit the present invention. As used in the embodiments of the present invention and the appended claims, the singular forms "a," "the," and "the" are intended to include the plural forms as well, unless the context clearly dictates otherwise.

[0058] The automatic launch and recovery device o...

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Abstract

The invention provides an automatic launch and recovery device and method based on an unmanned vehicle, which relates to the technical field of unmanned equipment transmission and reception. It can integrate the launch, recovery and storage of unmanned vehicles. Aerodynamic efficiency and payload capacity; the unit includes: an unmanned vehicle platform to provide the required power for the launch of the drone and during the recovery process to predict where the drone will land and move to it for recovery; automatic launch The device is used to carry and fix the unmanned aerial vehicle to be launched and automatically launch the unmanned aerial vehicle when the launch condition is met; the recovery device is used to complete the receiving work when the unmanned aerial vehicle lands, so as to realize the recovery of the unmanned aerial vehicle; the automatic launch device and recovery The devices are all installed on the unmanned vehicle platform. The technical scheme provided by the invention is applicable to the process of launching and recovering unmanned equipment.

Description

【Technical field】 [0001] The invention relates to the technical field of transmission and reception of unmanned equipment, and in particular, to an automatic launch and recovery device and method based on unmanned vehicles. 【Background technique】 [0002] The existing traditional UAV launch methods and recovery methods are designed separately. The launch methods include ground roll-off take-off, vertical take-off, hand-thrown take-off, catapult take-off, rocket-assisted launch, and aerial launch. The main methods of recovery include collision net recovery, sky hook, self-landing recovery, parachute recovery, stall recovery, etc. For these existing launch and recovery methods, for small and medium-sized fixed-wing UAV systems, it is difficult to achieve a balance in terms of economy, ease of use, safety, reliability and durability, automation and intelligence. The usage scenarios and application scope of the UAV system are summarized. [0003] At the same time, the existing...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/00B64F1/02B64F1/04
CPCB64F1/007B64F1/02B64F1/04
Inventor 王琨李金灵张传伟吕漪邴桂强
Owner AEROSPACE TIMES FEIHONG TECH CO LTD
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