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Airflow monitoring system for aircraft in atmosphere

A monitoring system and aircraft technology, applied in the field of aircraft monitoring, can solve the problems of large volume, heavy weight, and inability to perceive aircraft airflow

Active Publication Date: 2021-06-04
FUDAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the main problem with the pitot tube is that it cannot sense the airflow in all directions of the aircraft, and the pitot tube mainly adopts a mechanical structure, which is large in size and heavy in weight
At present, there is no ready-made product that can be directly used to provide aircraft with flight control of wind speed, wind direction and surrounding airflow conditions at the stratosphere and above altitudes.

Method used

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  • Airflow monitoring system for aircraft in atmosphere
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  • Airflow monitoring system for aircraft in atmosphere

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with drawings and embodiments. In the various figures, identical elements are indicated with similar reference numerals. For the sake of clarity, various parts in the drawings have not been drawn to scale. Also, some well-known parts may not be shown in the drawings.

[0028] In the following, numerous specific details of the present invention are described in order to provide a clearer understanding of the present invention. However, the invention may be practiced without these specific details, as will be understood by those skilled in the art.

[0029] figure 1 It shows the flow chart of information receiving, conversion and processing of the airflow monitoring system.

[0030] Such as figure 1 As shown, the anemometer chip converts the temperature signal of the chip area itself into electrical signal output of different frequencies, and the temperature of the chip itself is directly affected...

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Abstract

The invention belongs to the technical field of aircraft monitoring, and particularly relates to an airflow monitoring system for an aircraft in an atmosphere. The aircraft airflow monitoring system is mainly composed of an anemometer chip array and a pulse neural network sensor. The anemometer chip unit comprises a resonant network and cross-coupled transistors, and the power amplifier circuit comprises input matching, intermediate stage matching and output matching. The anemometer chips are distributed in a honeycomb shape to form an anemometer chip array, the anemometer chips can comprehensively and seamlessly cover the surface of the aircraft through the distribution mode, and information collection completeness is improved. The anemometer chip array converts the surface wind speed of a chip into a frequency signal, and the pulse neural network sensor analyzes the array output frequency signal through operation, so that the surrounding environment condition is identified, the flight state of the aircraft is judged, and the attitude of the aircraft is adjusted.

Description

technical field [0001] The invention belongs to the technical field of aircraft monitoring, in particular to an aircraft air flow monitoring system in the atmosphere. Background technique [0002] Unpredictable wind in the atmosphere is the main disturbance factor for the stable flight of multi-rotor aircraft. Unstable winds will seriously increase the difficulty of controlling the aircraft. If the wind speed is high, the aircraft will be in an extremely unstable state, and there may even be a risk of loss of control. Therefore, the estimation of the airflow around the aircraft is of great significance to the navigation, guidance and control of the aircraft. [0003] In modern aircraft, the motion characteristics of high-altitude atmospheric aircraft are greatly affected by the wind field of the environment. Therefore, real-time and accurate measurement of wind speed and wind direction is the premise of implementing long-term airborne and improving flight control quality. ...

Claims

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Application Information

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IPC IPC(8): G01P5/10G01P13/00
CPCG01P5/10G01P13/00
Inventor 马顺利许诺吴天祥曾超凡
Owner FUDAN UNIV
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