Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

A low-speed wind tunnel model flight experiment ground simulation training system

A ground simulation and training system technology, applied in the field of flight simulation, can solve the problems of inability to realize coordinated control training of three pilots, inconsistent response of control and response characteristic models, and inability to simulate different viewing angles, etc., to achieve high visual immersion and extensive engineering Application value, effect of increasing versatility

Inactive Publication Date: 2017-11-07
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
View PDF5 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the training of such flight operators, the aircraft model is generally used to carry out flight control training in the air. This method not only has high risk, high cost, and long preparation time, but also the control environment and control feeling are not consistent with the wind tunnel model flight experiment scene. The control and response characteristics of the aircraft model are not consistent with the response of the model to be used in the experiment, and realistic training cannot be realized; while the current general flight simulators are all simulators driven by a single pilot, and it is impossible to realize the coordinated control training of three pilots. Moreover, the visual display is also a single viewing angle, which cannot simulate the different viewing angles seen by different pilots during the wind tunnel model flight test

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 low-speed wind tunnel model flight experiment ground simulation training system
  • A low-speed wind tunnel model flight experiment ground simulation training system
  • A low-speed wind tunnel model flight experiment ground simulation training system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0035] In order to make the purpose, technical solution and advantages of the present invention clearer, the present invention will be further elaborated below in conjunction with the accompanying drawings.

[0036] In this example, see figure 1 and figure 2 Shown, a kind of ground simulation training system of low-speed wind tunnel model flight experiment, comprises integrated console 1, flight console, computer real-time solution system, visual system and audio system, described integrated console 1 and visual system are all connected to the Ethernet, the Ethernet is connected to the flight console and the real-time calculation system, the real-time calculation system is a multi-processor distributed real-time computing system interconnected through a reflective memory network, and the visual system is connected to the sound system.

[0037] 1. The integrated console 1 is the operation control center of the ground simulation training system, which is mainly used to set th...

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 ground simulation training system for a low-speed wind tunnel model flight experiment, which comprises an integrated console, a flight control console, a computer real-time computing system, a scene system and a sound system, wherein both the integrated console and the scene system are connected onto the Ethernet; the Ethernet is connected with the flight control console and the real-time computing system; the real-time computing system is a multi-processor distributed real-time computing system through a reflective memory network, and the multiple processors are mutually connected; and the scene system is connected with the sound system. The simulation training system disclosed by the invention can vividly simulate the experiment scene of the model for a six-degree of freedom unconstrained flight in the low-speed wind tunnel experiment section, and the problem of cooperative control training simultaneously by multiple pilots can be solved.

Description

technical field [0001] The invention belongs to the field of flight simulation, in particular to a ground simulation training system for low-speed wind tunnel model flight experiments. Background technique [0002] In the large-scale low-speed wind tunnel model flight experiment, the control and response of the model aircraft have the following characteristics: (1) Due to the use of a dynamic similar scale model, compared with the full-scale real aircraft flight, the dynamic response speed of the model is the same as that of the full-scale real aircraft. Compared with the real machine, it is much faster; (2) In the wind tunnel experiment section, six degrees of freedom are flying, and the extremely limited movement space requires the pilot to quickly control the position of the model; (3) Since the pilot is located in the measurement and control room and controls the movement of the model remotely , the lack of perception of the acceleration of the aircraft motion, which to ...

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): G09B9/00
CPCG09B9/00
Inventor 岑飞范利涛聂博文刘志涛孙海生
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products