KR20160013480A - Cockpit for aircraft simulation apparatus and the simulation method using the cockpit - Google Patents

Cockpit for aircraft simulation apparatus and the simulation method using the cockpit Download PDF

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Publication number
KR20160013480A
KR20160013480A KR1020140095082A KR20140095082A KR20160013480A KR 20160013480 A KR20160013480 A KR 20160013480A KR 1020140095082 A KR1020140095082 A KR 1020140095082A KR 20140095082 A KR20140095082 A KR 20140095082A KR 20160013480 A KR20160013480 A KR 20160013480A
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KR
South Korea
Prior art keywords
cockpit
simulation
model
position information
output lever
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Application number
KR1020140095082A
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Korean (ko)
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나호진
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한길씨앤씨 주식회사
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Priority to KR1020140095082A priority Critical patent/KR20160013480A/en
Publication of KR20160013480A publication Critical patent/KR20160013480A/en

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    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/12—Motion systems for aircraft simulators

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The present invention relates to a cockpit for a simulation apparatus, which is capable of perform various types of simulation by enabling adjustment of a position and the height of seats and a position of a control stick and a throttle. The present invention further relates to a simulation method using the cockpit. In the cockpit of the present invention, a control stick part and an output lever part are integrally formed, and the position of both can be adjusted depending on the type of the simulation target. Thus, the use of a single cockpit can allow a user to perform the simulation for various types. Therefore, the simulation can be easily performed and the costs required for the simulation remarkably decreases.

Description

TECHNICAL FIELD [0001] The present invention relates to a cockpit for a simulation apparatus and a simulation method using the cockpit,

The present invention relates to a cockpit for a simulation apparatus, and more particularly, to a cockpit for a simulation apparatus, and more particularly, to a cockpit for a simulation apparatus, The present invention relates to a cockpit for a simulation apparatus and a simulation method using the cockpit.

Generally, a simulator executes a computer program for outputting an image in accordance with a simulation image and an adjustment data, and a computer device executes an image applied to the simulation program on a screen. And recognizes the operation of the user control device such as the steering and the speed control device by the user, and converts the image according to the operation of the user control device in the screen projection image. Thus, by providing the effect that the user operates the actual device, the virtual experience game or the driving practice of the automobile or the airplane is performed by making the user feel as if the user actually controls the car, the motorcycle, .

An example of a simulator for the simulation of an aircraft in such a simulation is disclosed in Korean Patent No. 10-0986602 (hereinafter referred to as "Prior Art 1") "Simulator Motion Device" and Korean Patent No. 10-1350267 (Prior Art 2) And a cockpit-type horizontal and vertical variable air-flight simulation system.

The 'simulator motion apparatus' of the prior art 1 described above includes a base placed on a floor surface, a motion platform arranged on the top of the base, a motion reproducing apparatus for reproducing a virtual flight situation by moving the upper motion platform while being supported by the base, A cockpit and a controller installed on the upper part of the platform, a controller connected to the controller, and a host computer connected to the controller.

In the prior art 1 of the above-described construction, one or two cockpits are arranged in accordance with a model of an aircraft to be trained so that simulations on the aircraft can be performed, and then fixed on the motion platform to perform simulation training. Accordingly, the prior art 1 has a problem in that when the type of the aircraft to be trained is changed, the cockpit must be separated and relocated and reinstalled.

In order to solve such a problem, the 'cockpit longitudinally and horizontally variable aviation simulation system' of the prior art 2 has a rail on the upper surface of the motion platform so that the cockpit can be moved along the rails to vary the arrangement, The present invention discloses a technique for easily performing a simulation for a two-seat airplane by making it possible to easily vary the airplane in a horizontal arrangement.

However, in the case of the above-described prior art 2, since the position and the height of the cockpit itself, the position of the cockpit, and the position and height of the control lever and the output lever are fixed to each other, Can not be performed. This is also a problem that occurs in the prior art 1 as well.

SUMMARY OF THE INVENTION Accordingly, the present invention has been made keeping in mind the above problems occurring in the prior art, and it is an object of the present invention to provide a cockpit that can easily control the position and the height of the backrest, head restraint, The present invention provides a cockpit for a simulation apparatus and a simulation method using the cockpit, which can perform flight simulations for various types of aircraft such as F15 or F16 using one cockpit.

According to an aspect of the present invention, there is provided a cockpit for a simulation apparatus including: a base; A cockpit portion seated on the base; And a control unit for controlling the position of the pilot lever and the output lever unit according to the simulation target model, wherein the pilot lever is integrally formed with the pilot lever and the output lever unit, .

Wherein the cockpit portion includes a steering seat portion mounted on both sides of the steering shaft portion and the output lever portion so as to be positionally adjusted for each model; And a headrest portion for supporting the head of a trainee at an upper portion of the steering seat portion, wherein the headrest portion is configured to be vertically positioned according to the model to be simulated.

The headrest portion is configured to be vertically positioned according to the body of the trainee.

And the cockpit portion is configured to be adjusted in the forward and backward positions on the upper portion of the base according to the model to be simulated.

A simulation method using a cockpit for a simulation apparatus of the present invention includes a cockpit portion having a base, a cockpit seat having an output lever portion and a manipulating portion for varying position according to a model and a headrest portion, A simulation apparatus including a gauging section provided on a front surface of a cockpit section, the apparatus comprising: a model selection process of selecting a model to be simulated; A cockpit component position information extracting process of extracting position information of each component of the cockpit of the selected model; And controlling the position of each component of the cockpit according to the position information of the extracted cockpit component.

Wherein the cockpit constituent position information includes at least one of a front-back positional information of a cockpit seat constituting the cockpit section, a vertical position information of a headrest section mounted on an upper portion of the cockpit seat section, And up-and-down position information.

According to the present invention having the above-described configuration, it is possible to provide a simulation including one cockpit by adjusting the vertical position of the cockpit sheet, the pilot arm, the output lever portion, the fore and aft position of the cockpit, It is possible to select various models and perform simulation using the apparatus, thereby saving the cost and time required for the simulation.

1 is a perspective view of a simulation apparatus 1 according to an embodiment of the present invention.
2 is a perspective view of the cockpit unit 100 in the configuration of the simulation apparatus 1 of FIG.
3 is a view showing that the hydraulic cylinder 145 is structured such that the pilot trunk portion 140 and the output lever portion 150 are raised or lowered in a hydraulic or electric cylinder manner.
4 is a view showing the detailed configuration of the instrument display unit 200 in the simulation apparatus 1 of FIG.
5 is a flowchart showing a process of a simulation method using a cockpit for a simulation apparatus of the present invention.

Hereinafter, the present invention will be described in more detail with reference to the accompanying drawings showing embodiments of the present invention.

In the following description of the present invention, detailed description of known functions and configurations incorporated herein will be omitted when it may make the subject matter of the present invention rather unclear.

Embodiments in accordance with the concepts of the present invention can make various changes and have various forms, so that specific embodiments are illustrated in the drawings and described in detail in this specification or application. It should be understood, however, that the embodiments according to the concepts of the present invention are not intended to be limited to any particular mode of disclosure, but rather all variations, equivalents, and alternatives falling within the spirit and scope of the present invention.

It is to be understood that when an element is referred to as being "connected" or "connected" to another element, it may be directly connected or connected to the other element, . On the other hand, when an element is referred to as being "directly connected" or "directly connected" to another element, it should be understood that there are no other elements in between. Other expressions that describe the relationship between components, such as "between" and "between" or "neighboring to" and "directly adjacent to" should be interpreted as well.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. The singular expressions include plural expressions unless the context clearly dictates otherwise. In this specification, the terms "comprises ",or" having ", or the like, specify that there is a stated feature, number, step, operation, , Steps, operations, components, parts, or combinations thereof, as a matter of principle.

1 is a perspective view of a simulation apparatus 1 according to an embodiment of the present invention.

As shown in FIG. 1, the simulation apparatus 1 includes a cockpit 100, a meter display unit 200, and a base 400.

The base 400 includes a display unit 300 for outputting a simulation image, a cockpit unit 100, a meter display unit 200, and a display unit 300. Further, the base 400 is provided with a pair of front and rear rails 410 which are moved back and forth so that the cockpit 100 is positioned at a designated position according to the model.

The base 400 having the above configuration may be configured to be interlocked with an external swinging, rolling, or pitching device to perform an operation such as swing, rolling, pitching, or the like.

2 is a perspective view of the cockpit unit 100 in the configuration of the simulation apparatus 1 of FIG.

The cockpit 100 includes a control seat portion 110 on which the trainee sits and a headrest portion 120 formed on the control seat portion 110 to support the head of the trainee.

The headrest portion 120 is configured to be manually or automatically height-adjusted according to the selected model or the size of the user's body.

For example, the heights of the head rest portions 120 are manually or automatically adjusted according to the simulation of the F15 model or the F16 model, respectively. When the button for adjusting the height of the head rest portion 120 is pressed, the driving cylinder 121 of the hydraulic or electric type can adjust the height of the head rest portion 120 with respect to the control seat portion 110 .

Otherwise, when the simulation model is selected, the height of the headrest portion 120 is automatically adjusted by a device such as a hydraulic or electric cylinder.

The control seat portion 110 is mounted on the front and rear rails 410 formed on the upper portion of the base 400 so as to be movable back and forth. The front and rear positions on the base 400 are adjusted according to the selected simulation model, as described above. At this time, if the manual operation is performed manually, the position of the control seat portion 110 is manually moved on the front and rear rails and fixed using a fixing pin or a fixing means such as a bolt and a nut. Alternatively, in the case of being configured to be moved by an electric cylinder or a hydraulic cylinder, the user may control the forward / backward position on the base 400 of the control seat portion 120 in accordance with the model to be simulated by the control of the operation button do. When a model to be simulated is selected, the position of the control sheet portion 120 corresponding to the selected model is extracted, and a control unit (not shown) controls the entire simulation, The driving means such as the cylinder or the electric cylinder is driven to adjust the front and rear positions of the cockpit to the selected model to be simulated.

The steering shaft 140 and the output lever 150 are mounted on both sides of the steering seat 110. The steering shaft 140 and the output lever 150 may be manually or manually positioned depending on the selected simulation model. It is adjusted automatically.

In the case of manual adjustment, a plurality of position adjustment holes are formed in the upper and lower portions, and the height is adjusted by adjusting the position and then fixing the position using fixing pins or bolt and nut fixing means.

Alternatively, when an electric or hydraulic cylinder is provided, the upper and lower positions of the control lever 140 or the output lever unit 150 are adjusted by using an electric or hydraulic cylinder drive button.

When the model to be simulated is selected, the control lever 140 of the corresponding type and the output lever portion 150 of the output lever portion 150 are automatically controlled in such a manner that the positions of the control lever 140 and the output lever portion 150 are automatically adjusted. The upper and lower positions are extracted. Thereafter, a control unit (not shown) for controlling the entire simulation drives driving means such as a hydraulic or electric cylinder according to the extracted position information of the control lever 140 and the output lever unit 150, The position of the output lever portion 150 is automatically adjusted.

3 is a view showing that the hydraulic cylinder 145 is structured so that the control shaft portion 140 and the output lever portion 150 are raised or lowered in a hydraulic cylinder manner. Although not shown in FIG. 3, it is obvious that the output lever portion 150 may be structured such that the hydraulic cylinder 145 is mounted on the lower portion thereof and is moved up and down by the hydraulic pressure. In addition, the hydraulic cylinder 145 may have various configurations for ascending and descending, such as an electric cylinder, a screw bolt driven by an electric motor, and the like.

Fig. 4 is a diagram showing the detailed configuration of the instrument display unit 200 in the simulation apparatus 1 of Fig.

The instrument display unit 200 includes a graphical instrument display unit 210 at the center and a multifunction display unit (MFDS) 220 at both sides.

The graphical instrument display unit 210 includes a display device such as an LCD for simplifying the apparatus. The multifunction meter display unit 220 is provided with a display device such as an LCD at its center and multifunction buttons 225 to which various multifunctional control commands are assigned in the border area of the display device.

When the model to be simulated is selected, the instrument display unit 200 having the above-described configuration outputs a graphic instrument corresponding to the model selected by the simulation control unit (not shown) to the graphic instrument display unit 210, And outputs control commands corresponding to the multifunction buttons 225 for various controls formed at the edges of the multifunction instrument display unit 220. [

The graphic instrument 210 outputting the graphic instrument display unit 210 outputs an oil pressure gauge, a speed pressure gauge, an attitude gauge, an image switch, and the like.

The display of the multifunction meter display unit 220 displays various information such as a Weapons Display, a gun camera view, a communication stream, an air to ground radar, an air-to-air radar, (Air to Air Radar), Multiple Target Tracking Mode, Targeting Mode, Single Target Tracking Modes, Airborne or Ground Threat, Radar and IR Missile Warning, etc. The threat alarm indicator screen is displayed.

Referring again to FIG. 1, the simulation image display unit 300 outputs a simulation image corresponding to a field of view of a training object. That is, the real situation is simulated by outputting images of the ground and sky, moving images of the enemy, and the like.

5 is a flowchart showing a process of a simulation method using a cockpit for a simulation apparatus of the present invention.

1 to 3, the control seat portion 120 and the headrest portion 130 including the control lever 140 and the output lever portion 150, which are variable in position according to the selection of the model to be simulated, The simulation method by the simulation apparatus 1 including the cockpit unit 110 including the instrument display unit 200 and the simulation image display unit 300 and the base 400 can be classified into a model selection (S10), a cockpit component position information extraction process (S20), and a cockpit component position adjustment process (S30).

The model selection process S10 is a process of receiving a control command for a model to be simulated, such as F15 or F16, and extracting the model information.

As described above, after the model to be simulated is selected by receiving the control command inputted by the user and the simulation information about the model is extracted, the above-described cockpit constituent part position information extraction process S20 is performed, The position information of the cockpit constituent part is extracted from the simulation information. In this process, the front, back, and up and down positions of the control seat portion 110, the headrest portion 120, the control shaft portion 140, and the output lever portion 150 are extracted.

After the position information of the cockpit unit is extracted as described above, the cockpit unit position adjustment process (S30) is performed, and the positions of the cockpit units are adjusted by the automatic or manual method for performing the simulation.

Therefore, by configuring the cockpit to adjust the positions of the components so as to be suitable for various models, it is possible to simulate various models with a single cockpit by applying only the software for each model to one simulation device .

1: Simulation device
100: cockpit portion 110: pilot seat portion
120: head rest portion 140:
150: Output lever part 200:
210: graphic instrument display part 220: multifunction instrument display part
300: Simulation image display unit 400: Base

Claims (6)

The control lever and the output lever are integrally formed,
And the control lever and the output lever portion are adjusted in position in accordance with the model to be simulated.
The air conditioner according to claim 1,
A steering seat portion mounted on both sides of the steering shaft and the output lever portion so as to be positionally adjusted according to the type of the steering shaft; And
And a head rest portion provided at an upper portion of the steering seat portion so as to be vertically positioned according to the model to be simulated.
The headrest according to claim 2,
And the vertical position of the cockpit is adjusted according to the body of the trainee.
The air conditioner according to claim 1,
Wherein the cockpit is configured to be positioned at an upper portion of a base on which the cockpit unit is mounted, in accordance with the model to be simulated.
And a cockpit having a cockpit seat having an output lever portion and a head rest portion, the cockpit comprising:
A model selecting process for selecting a model to be simulated;
A cockpit component position information extracting process of extracting position information of each component of the cockpit of the selected model; And
And controlling a position of each component of the cockpit in accordance with the extracted position information of the cockpit component.
The system according to claim 5, wherein the position information of the cockpit comprises:
The position information of the cockpit sheet constituting the cockpit section, the position information of the headrest section mounted on the upper portion of the cockpit seat section, and the information of the upper and lower positions of the steering column section and the output lever section mounted on both sides of the cockpit seat sheet Wherein the simulation is performed by using the cockpit for a simulation apparatus.
KR1020140095082A 2014-07-25 2014-07-25 Cockpit for aircraft simulation apparatus and the simulation method using the cockpit KR20160013480A (en)

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KR1020140095082A KR20160013480A (en) 2014-07-25 2014-07-25 Cockpit for aircraft simulation apparatus and the simulation method using the cockpit

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KR1020140095082A KR20160013480A (en) 2014-07-25 2014-07-25 Cockpit for aircraft simulation apparatus and the simulation method using the cockpit

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110825236A (en) * 2019-11-21 2020-02-21 江西千盛影视文化传媒有限公司 Display system based on intelligent VR speech control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110825236A (en) * 2019-11-21 2020-02-21 江西千盛影视文化传媒有限公司 Display system based on intelligent VR speech control
CN110825236B (en) * 2019-11-21 2023-09-01 江西千盛文化科技有限公司 Display system based on intelligent VR voice control

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