Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

A wireless communication-based aircraft environmental parameter detection system and detection method

A technology of environmental parameters and wireless communication, applied in the field of detection, can solve the problems of reducing system weight and power consumption, complex data acquisition and transmission of space vehicles, etc., and achieve the effect of reducing power loss, reducing system equipment weight, and reducing power supply energy consumption.

Active Publication Date: 2018-11-23
CHINA ACAD OF LAUNCH VEHICLE TECH
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to overcome the deficiencies in the prior art, to provide a network layout design method suitable for space vehicles, with basically fixed nodes, definite network topology, and small number of nodes; using communication means based on wireless transmission technology to solve the problem of Data acquisition and transmission of complex structures of space vehicles, while reducing system weight and power consumption

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
  • A wireless communication-based aircraft environmental parameter detection system and detection method
  • A wireless communication-based aircraft environmental parameter detection system and detection method
  • A wireless communication-based aircraft environmental parameter detection system and detection method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0033] The present invention proposes a wireless communication-based aircraft environment parameter detection system and detection method. With the help of wireless communication technology, the sensor environment in the space vehicle can be realized through system network layout design, network scheduling management, time synchronization design, network topology layering, etc. Wireless transmission and processing of parameters. Using the time-division multiple access (TDMA)-based medium access control protocol, a network layout design method suitable for the characteristics of space vehicle nodes fixed, network topology, and small number of nodes is proposed; the system UTC time is used as the clock reference , clustered the network nodes, determined the time synchronization method of the 2-layer network structure, met the millisecond-level precision requirements, and solved the physical time synchronization problem of the system under the condition of high-speed data transmis...

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 an aircraft environment parameter detection system and detection method based on wireless communication. The detection system comprises a plurality of sensors, a plurality of wireless nodes, a main node, a data collection device and a network management node; each wireless node is connected with the corresponding sensor, receives a configuration command sent by the main node and is set to be a first-layer sub-node or a second-layer sub-node, receiving an environment parameter sent by the sensor connected therewith, and sending a control command to the sensor connected therewith; if being set to be the second-layer sub-node, the wireless node sends the received environment parameter to the first-layer sub-node, and sends to the main node through the first-layer sub-node; and the main node receives configuration information sent by the network management node, generates the configuration commands, sends to the wireless nodes, receives the environment parameters sent by the first-layer sub-nodes, and sends the environment parameters to the data collection device. According to the aircraft environment parameter detection system and detection method based on wireless communication, the complex structural data of an aircraft is wirelessly collected and transmitted.

Description

technical field [0001] The invention relates to a wireless communication-based aircraft environment parameter detection system and detection method, belonging to the detection field. Background technique [0002] With the development of space science and technology, countries around the world are accelerating the pace of outer space exploration, and constantly launching new aircraft and spacecraft. All military powers are focusing on the low-cost launch of space vehicles, high-efficiency mission execution, surveillance and early warning, New competitions have been launched in terms of rapid response and reuse, and the application range of space technology has been continuously expanded. The environmental parameter perception, processing and transmission technology applied to new space vehicles can realize the effective transmission and data processing of the aircraft's own flight status parameter information, space environment monitoring information, space battlefield inform...

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 Patents(China)
IPC IPC(8): H04W24/02G01D21/02G08C17/02H04W84/18
CPCG01D21/02G08C17/02H04W24/02H04W84/18
Inventor 李金龙刘建妥张德智张宏江陈朝霞刘洋曾星星胡倩刘小军
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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
Eureka Blog
Learn More
PatSnap group products