Flight simulator system with persistent overload simulation capability

A flight simulator and continuous technology, applied in simulators, simulation devices and instruments of space navigation conditions, etc., can solve the problems of poor flight simulation realism, low simulator fidelity, and lack of overload simulation capabilities. Achieve the effect of accurate overload component and better overload component

Active Publication Date: 2011-04-13
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA +1
View PDF3 Cites 31 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The fixed base flight simulator has less restrictions on the volume and weight of the simulator because of its fixed platform, and its visual simulation and cockpit simulation (cockpit layout, sound effects, etc.) Low, but it does not have the ability to simulate overload, the trained pilot (trainee) has no motion input, and the reality of flight simulation is poor
[0006] At present, the motion base flight simulator generally adopts the Stewart six-degree-of-freedom mechanism (see: Stewart D. Aplatform with six degree-of-freedom. Proceedings of the Institute for Mechanical Engineering. 1965, 180: 371-386) as its motion platform, bo

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
  • Flight simulator system with persistent overload simulation capability
  • Flight simulator system with persistent overload simulation capability
  • Flight simulator system with persistent overload simulation capability

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0050] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0051] see figure 1 As shown, a kind of flight simulator system with continuous overload simulation capability of the present invention has applied the equipment in the cockpit of a certain type of aircraft (such as visual module, instrument display module, drive start module, etc.), and trainee 1A Under the control of the aircraft, the various flight parameters of the actual flight will be output, and then the overload components will be extracted from the flight parameters, so as to realize continuous overload simulation. The flight simulator system of the present invention includes a flight simulator and an overload component model; the overload component model adopts the programming language of Microsoft Visual Studio VC98. The overload component model is stored in a PC; the PC is a modern intelligent electronic device that can automatically and high-spe...

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 flight stimulator system with persistent overload simulation capability. The flight stimulator system comprises a flight stimulator and an overload component model, wherein the overload component model is stored in a PC (Personal Computer); the flight stimulator comprises a nacelle, a rolling frame, a spiral arm, a weight balancing block, a base assembly, a first drive assembly, a second drive assembly, a third drive assembly and a fourth drive assembly, wherein the spiral arm, the nacelle and the rolling frame form a moving manned centrifugal platform; the moving manned centrifugal platform is driven by a motor in the base assembly and is also driven by the first drive assembly, the second drive assembly, the third drive assembly and the fourth drive assembly to realize persistent and non-instantaneous overload. A control method of the flight stimulator system comprises the following steps of: operating the flight parameters output by each device in the cockpit by a trainee; then, processing the flight parameters through the overload component model to as to obtain control parameters required by three-axial overload; and finally, accurately simulating three-axial persistent overload on the trainee by controlling the angular velocity of the spiral arm and the roll angle and the pitch angle of the nacelle.

Description

technical field [0001] The present invention relates to a ground flight simulation system, more particularly, refers to a ground flight simulation system capable of simulating three axial continuous overloads generated during actual flight. Background technique [0002] Modern high-performance aircraft will generate very large overloads during maneuvers, which have a very large impact on human physiology. The characteristic of this overload is that the peak value is relatively large, and the maximum overload can reach 9g (g is the acceleration constant of gravity, 9.81m / s 2 ); overload loading is fast, and the growth rate can reach 6g / s; the duration of overload is also longer, which can last for several seconds and may appear repeatedly. This long-lasting and large overload seriously affects the pilot's sense of space and ability to judge the situation during air combat maneuvers. The pilot may experience short-term black vision, spatial positioning illusion and even loss ...

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): G09B9/08
Inventor 王立新潘文俊
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP 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