Supercharge Your Innovation With Domain-Expert AI Agents!

Control method of aseismic airbag of fixed-wing unmanned target aerial vehicle

A technology of shock-absorbing airbags and control methods, applied in pump control, aircraft parts, mechanical equipment, etc., can solve problems such as damage to target drones, inability to meet shock-absorbing needs, and achieve the effect of meeting shock-absorbing needs

Active Publication Date: 2020-01-14
NO 60 RES INST OF GENERAL STAFF DEPT PLA
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the current airbag pressure is fixed, which cannot meet the shock absorption requirements of fixed-wing unmanned target drones at different altitudes, and may even cause damage to the target drone.

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
  • Control method of aseismic airbag of fixed-wing unmanned target aerial vehicle
  • Control method of aseismic airbag of fixed-wing unmanned target aerial vehicle
  • Control method of aseismic airbag of fixed-wing unmanned target aerial vehicle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0027] Below in conjunction with accompanying drawing, the implementation of the present invention will be further described:

[0028] The invention relates to a method for controlling a shock-absorbing airbag of a fixed-wing unmanned target drone. Specifically, it includes the following steps:

[0029] 1) After the fixed-wing unmanned target drone receives the landing signal, the unmanned target drone collects the parameter information at this time;

[0030] 2) Process the collected information and calculate the optimal internal pressure value of the shock-absorbing airbag;

[0031] 3) Collect the actual pressure inside the shock-absorbing airbag, and operate the inflatable fan to make the shock-absorbing airbag reach the optimal internal pressure;

[0032] 4) When the fixed-wing unmanned target drone lands, stop the fan.

[0033] The parameter information includes the height, temperature, fuel consumption, speed and acceleration of the fixed-wing unmanned target drone.

...

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 relates to a design of a control device of an aseismic airbag of a fixed-wing unmanned target aerial vehicle, relates to a control technology of the aseismic airbag of the fixed-wing unmanned target aerial vehicle, and is a solution scheme for realizing safe landing shock absorption of the fixed-wing unmanned target aerial vehicle. For realizing safe landing shock absorption of the fixed-wing unmanned target aerial vehicle, the aseismic airbag needs to be quickly inflated to the optimal state. The optimal internal pressure of the aseismic airbag which can achieve the best shock-absorbing effect is calculated in real time according to the height, temperature, fuel consumption, speed, acceleration and other information of the fixed-wing unmanned target aerial vehicle, and the optimal internal pressure is taken as a target pressure; the internal actual pressure of the aseismic airbag and the actual rotation speed of inflation fans are acquired meanwhile, the actual rotationspeed of the inflation fans are controlled by a control algorithm to enable the internal pressure of the aseismic airbag to quickly reach the optimal internal pressure; and finally, when the fixed-wing unmanned target aerial vehicle is landed, the control over the aseismic airbag is automatically stopped to prevent continuous inflation from damaging the device. The design is mainly used for safe landing shock absorption of the fixed-wing unmanned target aerial vehicle.

Description

technical field [0001] The invention relates to a control method for a shock-absorbing airbag of a fixed-wing unmanned target drone, which is mainly used for the safe landing of the fixed-wing unmanned target drone for shock absorption. Background technique [0002] During the landing and recovery process of the fixed-wing unmanned target drone, when the fixed-wing unmanned target drone opens the parachute, the shock-absorbing airbag must be opened in time to ensure that the shock-absorbing airbag can play a shock-absorbing role when the fixed-wing unmanned target drone lands. In order to prevent the fixed-wing unmanned target drone from being too impacted at the moment of landing, causing damage to the body and causing huge losses. At present, most of the shock-absorbing airbags of fixed-wing unmanned target drones use the method of igniting the explosives inside the gasbag, so that the airbags are inflated instantly, so as to ensure that the fixed-wing unmanned target dron...

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
IPC IPC(8): B64C25/58F04D27/00
CPCB64C25/58F04D27/008
Inventor 陈剑王德明毛师彬
Owner NO 60 RES INST OF GENERAL STAFF DEPT PLA
Features
  • R&D
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More