High-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles and ejection chute

A kind of unmanned aerial vehicle, small and medium-sized technology, applied in the field of high-speed parachute drop system and catapult parachute, can solve the problems of distance deviation, deviation from the predetermined target point, long time of parachute opening process, etc., achieve process controllability, shorten recovery time, The effect of ensuring landing accuracy

Pending Publication Date: 2018-06-12
沈观清 +1
View PDF12 Cites 14 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] The problem is not only the distance offset, the main difficulty is that the entire landing recovery process is uncontrollable
This is unacceptable for military drones
[0011] To sum up, in the existing technology, there are problems that the unmanned aerial vehicle parachute height cannot be lowered, the parachute opening process takes a long time, and the aircraft deviates from the predetermined target point after landing.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • High-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles and ejection chute
  • High-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles and ejection chute
  • High-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles and ejection chute

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0063] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0064] Design principle of the present invention.

[0065] Such as figure 1 Shown is the principle diagram of the high-precision parachute of the present invention. figure 2 There are two circular areas in the center, from the outside to the inside, there is a pre-entry area with a radius of 100 meters and a height of 80 meters; a parachute opening area with a radius of 50 meters and a height of 50 meters; figure 2 It also indicates the location of the ejection airgun parachute opening: on a circle with a radius of 50 meters at low altitude; it also shows that the forward direction of the ejector and the wind direction are opposite when the parachute is open against the wind; it also indicates that the speed when the parachute is opened is low speed : 8 meters per second, and the speed at which the aircraft enters the pre-entry area is 7 meters per second...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a high-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles and an ejection chute. The high-speed parachute landing system and method for medium-and-small-sized unmanned aerial vehicles is characterized by comprising a ground control station control unit, an environment and plane information data acquiring unit, a flight control system, a data processing and executing information generating unit and an ejection sequence starting unit. The method comprises the following steps: setting height parameters and speed parameter of low-altitude and low-speed parachute opening of an unmanned aerial vehicle; flying the unmanned aerial vehicle to the sky above a specific landing region and receiving a ground station command; determiningthe landing region and entering the region according to a specific path; and starting a control system to open a parachute by ejection and landing. The ejection chute comprises a parachute and ejection gas cylinder guns which are mounted at four corners of the parachute. By low-altitude parachute opening, vertical landing time of the unmanned aerial vehicle after the unmanned aerial vehicle enters the landing region is saved by 50%; the whole parachute opening process is automated, a landing preset target point of the unmanned aerial vehicle is positioned accurately; and by parachute openingthrough ejection, the parachute opening speed is increased.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle recovery, in particular to a high-speed parachute system, method, and ejection parachute for the recovery of small and medium-sized unmanned aerial vehicles. Background technique [0002] The parachute recovery method is a routine recovery method for small and medium-sized UAVs. The scope of application of small and medium-sized UAVs is very wide, but the recycling of small and medium-sized UAVs is always a major obstacle to the application of UAVs. [0003] Since small and medium-sized UAVs are often used in forests, mountains, rivers and lakes, alpine regions and offshore areas, take-off and landing recovery must have a variety of take-off and recovery technologies due to landform and condition constraints. [0004] The parachute recovery technology usually uses the parachute carried by the drone to open the parachute in the air, and then slowly descend to the ground. When the ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B64D17/54B64D17/64B64D17/80
CPCB64D17/54B64D17/64B64D17/80B64U70/83
Inventor 沈观清春燕
Owner 沈观清
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products