Electric aircraft positioning system based on space solar power stations and control method thereof

A technology of space solar energy and electric aircraft, applied in electromagnetic wave systems, three-dimensional position/lane control, electric vehicles, etc., can solve difficult problems, aircraft load limit, aircraft evaporation, etc., to avoid carbon emissions and high positioning accuracy , the effect of zero emissions

Inactive Publication Date: 2015-07-29
CIVIL AVIATION UNIV OF CHINA
View PDF1 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Relevant experts believe that the personnel on board manually turned off the aircraft positioning device, which caused the failure of the aircraft positioning function, and made the aircraft in the MH370 incident disappear, and it is still not found.
The current aircraft positioning mainly relies on the satellite-based GPS system. Through the MH370 incident, it was discovered that the biggest problem with this system is: if the transmitter closes the signal transmission, the control terminal will not be able to perform positioning. This problem is still difficult to solve with current technical means
However, the main problem of electric aircraft is endurance. Although with the continuous improvement of solar cell efficiency, intercontinental flight can be realized, but it cannot be used for commercial purposes due to the limitation of aircraft load.

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
  • Electric aircraft positioning system based on space solar power stations and control method thereof
  • Electric aircraft positioning system based on space solar power stations and control method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0024] The precise positioning system and control method for electric aircraft based on space solar power plants provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0025] Such as figure 1 As shown, the electric aircraft precise positioning system based on the space solar power station provided by the present invention includes a control terminal 1 and a receiving terminal 2, and the control terminal 1 includes a plurality of space solar power stations 3, a plurality of power transmitters 4 and a plurality of positioning Information transmitter 5, wherein the space solar power station 3 is a geostationary satellite with a solar power station, on which a control device is provided; the power transmitter 4 and the information transmitter 5 are arranged on the space solar power station 3, and the space solar power station 3 and The power transmitter 4 is connected with the information transm...

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

Disclosed are an electric aircraft positioning system based on space solar power stations and a control method thereof. The electric aircraft positioning system based on the space solar power stations comprises a control end and a receiving end, wherein the control end is composed of a plurality of the space solar power stations, a plurality of power transmitters and a plurality of positioning information transmitters, wherein the space solar power stations are geo-stationary satellites with solar power stations; the power transmitters and the information transmitters are arranged on the plurality of space power stations; the receiving end comprises a plurality of power receivers, a plurality of groups of high-capacity storage batteries and a plurality of positioning information receivers, and the power receivers, the high-capacity storage batteries and the positioning information receivers are arranged at the top and inside every electric aircraft and connected with one another to supply power for the electric aircraft. The electric aircraft positioning system based on the space solar power stations and the control method can achieve remote wireless power supply of the electric aircrafts and determine the spatial coordinates of the electric aircrafts in real time, and has the advantages of being energy-saving, environmentally friendly and accurate in positioning.

Description

technical field [0001] The invention belongs to the technical field of aircraft positioning, and in particular relates to an electric aircraft precise positioning system and control method based on a space solar power station. Background technique [0002] With the development of the civil aviation industry, more and more people choose to travel by air. However, with the increase in the number of flights and the intensification of terrorist activities, the issue of aircraft safety has increasingly attracted public attention. In particular, the occurrence of the Malaysia Airlines MH370 incident in 2014 once again aroused people's high attention to flight safety issues. Relevant experts believe that the personnel on board manually turned off the aircraft positioning device, which caused the failure of the aircraft positioning function, and made the aircraft in the MH370 incident disappear, and it is still not found. The current aircraft positioning mainly relies on the satel...

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): G05D1/10H02J17/00H02J7/00
Inventor 刘国光武志玮武志锴
Owner CIVIL AVIATION UNIV OF CHINA
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