KR102032831B1 - Simulator system for emergency escape training of pilot by using parachute - Google Patents

Abstract

The present invention is to solve the problems of the prior art, the present invention of the present invention pilot aircraft escape escape training simulator system using a parachute simulated the process of pilots on board the aircraft trying to escape in the air Trainees can experience the entire process of emergency escape of the aircraft from the emergency exit by the emergency exit to the free fall by the parachute at once, and the flight dynamics of the parachute by the free fall from above This modeling and simulator technology is applied, and the virtual reality is realized by 3D image rendering and precise sensor control, so that the trainee can experience the situation as realistic as possible and train on various situations that can occur during the emergency escape of the aircraft. Scenarios can be set up, and various The present invention relates to a parachute simulator system that provides a function.

Description

Simulator system for emergency escape training of pilot by using parachute

The present invention relates to an aircraft pilot emergency escape training simulator system using a parachute, and more specifically, the present invention is an emergency escape to enable pilots on board the aircraft to simulate and experience the process of attempting an emergency escape from the air. It is a simulator system.

In addition, the present invention is an emergency escape simulator system that allows the trainee to experience the entire process of the emergency escape of the aircraft from the emergency escape by the injection seat to the free fall by parachute at once.

In addition, the present invention is applied to modeling and simulation technology reflecting the flight dynamic characteristics of the parachute due to free fall in the air, the virtual reality by the three-dimensional image rendering and precise sensor control, the trainees experience the situation as realistic as possible It is an emergency escape simulator system using a parachute.

In addition, the present invention is a parachute simulator system capable of setting a training scenario for various situations that may occur during an emergency escape of the aircraft, and provides a variety of functions for the evaluation of the training carried out.

It takes a lot of time now to train pilots, and the loss of a pilot in an accident is not only a simple loss of life, but also a big loss nationally.

In Korea, pilot training is limited to the Air Force and civilian airlines, and the pilot training conducted by the Air Force is the most systematic in terms of quality and quantity.

At this time, it is about emergency escape that is just as important as mastering the operation of the aircraft in pilot training.

The emergency evacuation training system currently operated by the Air Force is divided into parachute pilot training, which is limited in function by injection experience using an injection seat introduced from overseas and parachute pilot training.

However, the simulator used for the parachute pilot training is a 3D virtual reality-based simulation training system for emergency escape, parachute descent, and landing stage training in preparation for the occurrence of an aircraft emergency during pilot mission.

In addition, the free fall parachute control simulator exists in Korea, but the lack of fidelity of the free fall and parachute flight dynamics modeling results in poor training effect, and there is no simulator system for emergency escape training using virtual reality environment in Korea. .

Therefore, by conducting emergency escape training during the pilot training period, which cannot be experienced except in actual aircraft emergency situations, various technologies have been developed for the purpose of enhancing survivability by improving the pilot's parachute control. The following are the prior art in this regard.

1. Republic of Korea Patent Publication No. 10-2014-0066934 drop training simulator and its operation method The invention of the prior art document 1 relates to a drop training simulator and a method of operation thereof capable of performing a parachute descent training on the ground as in the real world. However, the invention of the prior art document 1 has a disadvantage in that the parachute control training by parachute escape is possible, but the function is limited to use as an emergency escape training of the pilot because there is no function to eject from the aircraft cockpit. 2. Republic of Korea Patent Publication No. 10-156408 Parachute control simulation training device Invention of the prior art document 2 relates to a training device that can provide a type of environment most similar to the external environment that can be generated during the flight process during the simulation simulation of the parachute and train appropriate and sophisticated parachute control accordingly. will be. However, the invention of the prior art document 2 has a disadvantage in that the parachute control training by the parachute escape is possible, but the function is limited to use as an emergency escape training of the pilot because there is no function to eject from the aircraft cockpit. 3. Republic of Korea Patent Publication No. 10-1483105 A flight simulator device equipped with a parachute descent training mode function and its control method The invention of the prior art document 3 relates to a flight simulator device having a parachute training mode function for maximizing a training effect and a control method thereof. However, the invention of the prior art document 3 has a disadvantage that the actual experience effect that the trainees get less because the training proceeds depending on the video screen provided by the display.

The present invention is to solve the above problems, it is an object of the present invention to provide a parachute simulator system that allows pilots on board an aircraft to simulate and experience the process of attempting an emergency escape in the air.

In addition, an object of the present invention is to allow the trainee to experience the entire process of emergency escape of the aircraft from the emergency escape by the injection seat to the free fall by the parachute at once.

In addition, the present invention is applied to modeling and simulator technology reflecting the flight dynamic characteristics of the parachute due to free fall in the air, the virtual reality by the three-dimensional image rendering and precise sensor control, the trainees experience the situation as realistic as possible The purpose is to make it.

In addition, an object of the present invention is to enable the setting of training scenarios for various situations that may occur during an emergency escape of the aircraft, and to provide various functions for evaluating the carried out training.

In order to achieve the above object, the present invention pilot aircraft escape simulator training system using a parachute,

A frame unit 100 which provides a training space for the trainees and supports other devices;

An emergency injection unit 200 for providing an emergency escape situation to the trainees;

An HMD 300 worn by the trainees to provide the trainees with a video image according to the falling situation;

A parachute harness 400 worn by the trainee;

A motion control line 500 in which movement is controlled by a drive control system to make the trainee feel a parachute descent situation;

A parachute control line 600 for providing a parachute steering signal to the drive control system 800 after the emergency escape;

A motion sensor unit 700 for extracting the posture of the parachute drop trainee;

Sliding control of the emergency injection unit 200 to provide an emergency escape effect of the trainees, and to the control signal provided from the simulation engine / image generator computer 900 to make the trainees feel the parachute drop situation Drive control system 800 for controlling the movement of the motion control line 500 and the parachute control line 600 according to;

A simulation engine / image generation computer 900 for generating 3D images and modeling and simulation functions such as free fall and parachute dynamics;

An instructor control unit including an instructor control computer for creating and editing various training scenarios before training, simulator control by setting a training situation during training, and debriefing (evaluation by data storage / replay) after training. 1000); characterized in that it comprises a.

As described above, the pilot system for piloting emergency escape of aircraft using the parachute of the present invention enables pilots on board an aircraft to simulate and train the process of attempting emergency escape in the air, thereby allowing pilots to escape from the aircraft. Increase the success rate when attempting to reduce pilot's life loss.

In addition, the present invention allows the trainee to experience the entire process of the emergency escape of the aircraft from the emergency escape by the injection seat to the free fall by the parachute at one time, the emergency escape training of the aircraft pilot compared to the prior art limited only to parachute training More suitable for.

In addition, the present invention is applied to modeling and simulator technology reflecting the flight dynamic characteristics of the parachute due to free fall in the air, the virtual reality by the three-dimensional image rendering and precise sensor control, the trainees experience the situation as realistic as possible This increases training effectiveness and increases pilot survival, reducing loss of life.

In addition, the present invention can set the training scenarios for various situations that can occur during the emergency escape of the aircraft, and provides a variety of functions for evaluating the training carried out not only provide a high training effect to the trainees but also personalized training It also becomes possible.

1 is an exemplary view illustrating a configuration of a pilot system for emergency escape training of an aircraft pilot using a parachute of the present invention.
Figure 2 is a block diagram of the configuration of a pilot pilot flight escape training system using the parachute of the present invention.
Figure 3 is an illustration of an emergency injection unit of the aircraft pilot emergency escape training simulator system using the parachute of the present invention.
Figure 4 is a flow chart of the emergency injection unit operation of the pilot pilot flight escape training system using the parachute of the present invention.
Figure 5 is a flow chart of the injection cockpit operation of the aircraft pilot emergency escape training simulator system using the parachute of the present invention.
Figure 6 is an exemplary view of the three-dimensional cockpit boarding screen of the aircraft pilot emergency escape training simulator system using the parachute of the present invention.
Figure 7 is an exemplary view of the three-dimensional terrain DB rendering screen of the aircraft pilot emergency escape training simulator system using a parachute of the present invention.
8 is a block diagram of a drive control system of an aircraft pilot emergency escape training simulator system using the parachute of the present invention.
9 is a control flowchart of a drive control system of an aircraft pilot emergency escape training simulator system using a parachute of the present invention.
10 is a perspective view of the reaction force generation unit of the pilot system for emergency escape training using the parachute of the present invention.
FIG. 11 is a side view and a part view of a reaction force generating unit of an aircraft pilot emergency escape training simulator system using a parachute of the present invention. FIG.
12 is a block diagram illustrating the simulation engine / image generation computer configuration of the pilot system for piloting an emergency escape of an aircraft pilot using a parachute of the present invention.
FIG. 13 is a diagram illustrating a parachute dynamic coordinate system of an emergency pilot training system for piloting an aircraft using a parachute of the present invention. FIG.
14 is a diagram showing the parachute characteristics data of the pilot system for emergency escape training using the parachute of the present invention.
15 is a view showing an inverter for controlling the blower of the simulator pilot escape training training system using the parachute of the present invention.

An embodiment of the present invention as described above will be described in detail with reference to FIGS. 1 to 15.

The pilot system for piloting emergency escape of aircraft using the parachute of the present invention enables pilots on board an aircraft to simulate and train the process of attempting emergency escape in the air, when the pilot attempts to escape from the aircraft. The invention provides an effect of reducing the loss of pilot life by increasing the success rate.

Therefore, the present invention will be described in detail with reference to the drawings the embodiment pilot aircraft escape training training system using a parachute.

Referring to Figures 1 to 3, the pilot pilot flight escape training system using the parachute of the present invention (hereinafter referred to as "system") is the frame portion 100, the emergency injection unit (200), HMD ( 300, parachute harness 400, motion control line 500, parachute control line 600, motion sensor unit 700, drive control system 800, simulation engine / image generation computer 900, instructor control unit ( 1000).

The system 10 of the present invention has been developed to improve the limited aircraft emergency escape training system of the prior art, and the above configurations of the present invention organically fuse and apply the component technologies of the coupling and simulator to the emergency pilot training of the aircraft pilot. To maximize the effectiveness of each function, the following key technologies were applied.

1) Virtual Reality technology that provides realistic 3D image information

2) Free fall of parachute and dynamic modeling and simulation of parachute

3) Motion sensor technology incorporating Gyro sensor into HMD and measuring trainee's parachute control and trainee's descent posture

4) Drive control technology to realize the process from the pilot's cockpit escape to the parachute

5) Training scenario setting and training result analysis and evaluation technology

Referring to FIG. 1, the frame part 100 provides a training space to an education trainee and includes a plurality of support frames 110, an upper frame 120, and a lower frame 130 as a structure for supporting other devices. It is configured by.

Here, one side of the plurality of support frames 110 is connected to the upper frame 120 to support the upper frame 120, the other side is connected to the lower frame 130.

The plurality of support frames 110 are characterized in that at least four or more are formed to function as a support rod.

The upper frame 120 is connected to the plurality of support frames 110 and the drive control system 800 is formed on one side.

The lower frame 130 is connected to the plurality of support frames 110 and the injection guide groove 131 to which the injection sliding part 220 can move is formed.

The frame unit 100 including the plurality of support frames 110, the upper frame 120, and the lower frame 130 as described above functions as a structure that provides training space to the trainees and supports other devices. Done.

The support frame 110, the upper frame 120, the lower frame 130 is applied to a metal material with excellent mechanical properties that can sufficiently withstand the vibration and shock generated during training while supporting the load of trainees and other devices It is desirable to.

3 and 4, the emergency injection unit 200 is configured to implement the first seat injection operation in the parachute simulator system of the present invention when the aircraft pilot attempts emergency escape in an actual situation. Including, the injection cockpit 210 and the injection sliding portion 220 is configured.

Here, the injection cockpit 210 is formed in the same shape as the aircraft cockpit to provide a space for the trainees seated, and the injection pre-operation to raise and lower the seated trainees to a certain height on the injection sliding part 220 The configuration to perform may be configured to include an emergency escape switch 211 as shown in FIG.

In addition, the injection sliding part 220 is formed as shown in Figure 1, the lifting and lowering guide grooves 221 for guiding the rising and falling of the injection cockpit 210, when selecting the trainee emergency escape (eg : Press emergency escape switch 211) The backward sliding movement on the injection guide groove 131 formed in the lower frame 130 provides an emergency escape effect to the trainees.

More specifically, the injection cockpit 210 raises the trainees by a predetermined height through the injection pre-operation as shown in the left figure of FIG. 4. That is, the injection cockpit 210 ascends the trainee by moving up and down along the lifting and lowering guide grooves 221 formed in the injection sliding part 220 to a certain height. Then, when the trainee selects the emergency escape (press the emergency escape switch 211), as shown in the right picture of Figure 4 the injection sliding portion 220 on the injection guide groove 131 formed in the lower frame 130 The trainee who moves up to a certain height by sliding backward moves away from the injection cockpit 210 to provide an emergency escape effect to the trainee.

In this case, the driving force for sliding backward movement on the injection guide groove 131 formed in the lower frame 130 is provided by the injection drive unit 840 of the drive control system 800 to be described later.

 Referring to FIG. 1, the HMD 300 is a kind of training goggles (Head mounted Display) worn by the trainees so that the trainees can feel the situation similar to the real situation through the visual effect.

Here, the image information provided by the trainee through the HMD (300) is generated by the simulation engine / image generation computer 900, the image information combines the pilot's line of sight and flight dynamics of the parachute in the air. As the 3D image information, the trainee can experience the virtual reality related to the descent through the parachute.

In addition, the HMD 300 has a built-in speaker or earphone function to provide not only 3D image information, but also auditory information, thereby inserting sound effects related to training to increase the immersion of training or guide or instruct the voice of a training instructor. Allow them to conduct training while listening.

Therefore, when the trainee wears the HMD 300 for training and is seated in the emergency injection unit 200, the trainee is first provided with a three-dimensional cockpit boarding screen as shown in FIG. During training, a 3D terrain DB rendering screen as shown in FIG. 7 is provided to increase training immersion to trainees.

The HMD 300 may further include a plurality of gyro sensors. The HMD 300 may further include posture information of a trainee required to correct and maintain an aerial flight posture according to image information according to a falling situation. Detect and create

The parachute harness 400 is worn by trainees for the parachute training, and the parachute harness 400 of the present invention is worn by the trainees as if the actual harness is the equipment for connecting the pilot and the parachute, and the parachute harness 400 is illustrated in FIG. As shown in FIG. 1, the motion control line 500 is connected to allow the trainees to feel the parachute drop situation according to the motion control line 500 movement control by the drive control system 800.

Since the motion control line 500 has one side connected to the parachute harness 400 and the other side connected to the drive control system 800, the motion control line 500 movement control by the drive control system 800 is parachute as it is. The harness 400 is delivered to the trainee to feel the parachute descent situation.

The parachute control line 600 is composed of two left and right, as shown in Figure 1, trainees hold one by one for both hands to control the parachute, the trainees fall according to the strength of the force pulling the parachute control line 600 (falling) The image information of which direction is changed is provided by the simulation engine / image generating computer 900 to the HMD 300 so that the trainee feels the drop situation change according to the adjustment of the parachute control line 600.

In addition, in the air descent situation through the actual parachute when the control to pull through the parachute control line 600, you will feel the reaction force transmitted from the parachute. The present invention also comprises a control line sensor 820 and the reaction force generating unit 830 in the drive control system to provide the trainee with a reaction force that can be felt in such a real situation to the strength of the force that the trainee pulls the parachute control line 600 Produces reaction force according to the parachute control line 600 to provide.

The motion sensor unit 700 extracts the descent posture information of the trainee and transmits it to the instructor control computer. The training posture drop information of the trainees is used as the trainee's descent training evaluation data.

The drive control system 800 sliding control the emergency injection unit 200 to provide an emergency escape effect of the trainees, motion control line 500 to train the trainees to feel the parachute drop situation. And control the movement of the parachute control line 600.

To this end, as shown in FIGS. 2 and 8, the drive control system 800 moves the trainee's posture up and down / backwards so that the trainee who escapes the train can feel the parachute drop situation of the motion control line 500. Trainee motion control unit 810 for controlling the movement,

The trainee detects the pull when the parachute pulls the control line, and the control line sensor 820 provides a detection signal to the reaction force generator 820 and the simulation engine / image generating computer 900 when the pull is detected;

Reaction force generation unit 830 for generating a reaction force generated in the opposite direction to the pulling force when the trainee pulls the parachute control line when providing a detection signal from the control line sensor 830,

When selecting the trainee emergency escape for sliding the injection sliding part 220 of the emergency injection unit (200) on the injection guide groove 131 of the lower frame 130 to provide an emergency escape effect to the trainees It is configured to include an injection drive 840.

Referring to FIG. 10, the trainee motion control unit 810 is formed in plural on the upper frame 120, and each trainee motion control unit 810 is connected to the parachute motion control line 500, and the servo motor, It includes a speed reducer, a bearing, a carpooling, and the like to make the trainee feel the parachute drop situation by raising or lowering the parachute motion control line 420 by forward rotation and reverse rotation.

Referring to FIG. 11, when the trainee receives a detection signal from the control line sensor 820 that detects a force pulling the parachute control line 600, the trainee pulls the parachute control line 600. It is a configuration that generates reaction force that reacts to a force, and includes a reaction force generator, a reaction sensor, and a control line link.

The reaction force growth value is fixed to the length of the reaction sensor corresponding to the displacement sensor (LVDT: Linear variable differential transformer) through the spring balance of the built-in spring spring, pulling the parachute control line 600 connected to the control line connecting ring It is to create a reaction force that counters the trainee's power.

As shown in FIG. 12, the simulation engine / image generating computer 900 calculates a modeling value of free fall and dynamic characteristics of a parachute and provides the driving control system 800 to a 3D virtual image according to the modeling value. It is configured to include a simulation engine unit 910, image generation unit 920, database unit 930 to generate and transmit to the HMD 300 to proceed with the parachute descent training.

The simulation engine unit 910 is an arithmetic device that processes simulation situations such as free fall of the parachute and dynamic modeling values of the parachute shown in FIGS. 13 and 14, environmental modeling values such as wind, and malfunction of the parachute. The control signal according to the processing is provided to the drive control system 800.

The image generator 920 loads and renders image data including a 3D object model such as a parachute, an aircraft, a character, and terrain information from the database unit 930 according to a processing situation of the simulation engine 910. Rendered image data reflects day and night changes, weather effects such as snow, clouds, rain and storms, and various predictable special effects, and displays 3D image information that changes according to the trainee's gaze and parachute control. The graphics processing module is generated in real time and provided to the trainees wearing the HMD (300).

In addition, the image generating unit 920 needs to apply a plurality of expensive graphics modules which have better performance than a general PC graphics module because of the high capacity graphics processing.

The database unit 930 is a storage device for storing modeling values and image information generated by the simulation engine unit 910 and the image generating unit 920. Since the 3D modeling values and the image information are high capacity, the server PC is preferably used. The high-capacity storage used for the

Referring to FIG. 1, the instructor control unit 1000 is a training control seat used by an instructor, not a trainee, includes an instructor control computer 1010 and an instructor monitor 1020, and further includes an instructor microphone 1030. Can be configured.

The instructor control computer 1010 generates or loads various training scenarios executed by the trainee, and provides a function of editing detailed settings of the generated or loaded training scenarios.

On the other hand, the instructor can quickly stop the training being carried out through the instructor control computer 1010 to protect the trainees.

The instructor control computer 1010 is based on the trainee drop posture extraction data acquired through the motion sensor unit 700 during the training and the parachute dynamic data that the trainee pulled and manipulated the parachute control line 600 as the training time elapsed. The ability to assess and analyze trainees' training results provides trainees with a high level of training effectiveness, as well as personalized training.

The instructor monitor 1020 is a monitor that the instructor monitors the image information provided to the HMD 300, the image information in the three-dimensional space that the trainees parachute descent in the air, the instructor monitors the actual appearance of the trainees to shoot from the surrounding camera It is a constituent means for comprehensively and objectively grasping the trainee's training status while watching (1020).

In addition, the instructor may use the instructor microphone 1030 to explain the training situation to the trainee who is immersed in the virtual reality by the HMD 300, or give appropriate instructions or guidance to the trainee so that the trainee can concentrate more on the training process. do.

The training monitor 1040 is a monitor that non-trainees including a training instructor do not watch, and the training monitor 1040 is an image provided to the HMD 300 of the trainee who is currently training in the system 10. The information is also provided to non-trainees to observe the trainees 'eyes on the trainees and to assist them in analyzing and evaluating the trainees' training results when the training is over.

At this time, since the trainee can only obtain the virtual image information from the worn HMD (300), it is difficult to obtain the objective information about their parachute descent posture, install a camera to shoot the trainee around the system 10 of the present invention This can assist in the analysis and evaluation of the training results after the end of training.

Referring to FIG. 15, the parachute simulator system of the present invention may further include a blower 1100 illustrated in FIG. 1.

This is a kind of fan that creates a wind for the trainees to enhance the wind experience to be hit in the air during the training of parachute descent, and is installed in a plurality for an effective blowing effect.

Here, the blower 1100 is a parachute drop training effect experienced by the trainer by changing the strength and direction of the blow in real time according to the flight dynamics simulation of the parachute processed by the simulation engine / image generation computer 900 over time It is a configuration to increase.

In particular, the blower 1100 increases the training effect of the training parachute drop when the blower 1100 is operated in conjunction with the flow of training scenarios provided by the simulation engine / image generating computer 900 and the control of the trainee's parachute control line. You can do it.

The parachute simulator system 10 of the present invention described above allows the trainee to experience the entire process of the emergency escape of the aircraft from the emergency escape by the emergency injection unit 200 to the fall by the parachute at once, so that the parachute training Compared to the prior art, which is limited only to the pilot, the invention is more suitable for the pilot's emergency escape training and effective for the pilot's emergency escape training, thus increasing the survival rate of the pilot's actual escape. The invention is highly industrially available because it protects human life and prevents the loss of national human resources.

10: system
100: frame portion
200: emergency injection unit
300: HMD
400: Parachute Harness
500: Motion Control Line
600 Parachute Control Line
700: motion sensor
800: drive control system
900: simulation engine / image generating computer
1000: Instructor Control Department
1100: blower

Claims (7)

In the aircraft pilot emergency escape training simulator system using a parachute,
A frame unit 100 which provides a training space for the trainees and supports other devices;
An emergency injection unit 200 for providing an emergency escape situation to the trainees;
An HMD 300 worn by the trainees to provide the trainees with a video image according to the falling situation;
A parachute harness 400 worn by the trainee;
A motion control line 500 in which movement is controlled by a drive control system to make the trainee feel a parachute descent situation;
A parachute control line 600 for providing a parachute steering signal to the drive control system 800 after the emergency escape;
A motion sensor unit 700 for extracting the posture of the parachute drop trainee;
Sliding control of the emergency injection unit 200 to provide an emergency escape effect of the trainees, and to the control signal provided from the simulation engine / image generating computer 900 to the trainees to feel the parachute descent situation Drive control system 800 for controlling the movement of the motion control line 500 and the parachute control line 600 according to;
A simulation engine / image generation computer 900 for generating 3D images and modeling and simulation functions such as free fall and parachute dynamics;
An instructor control unit including a instructor control computer for creating and editing various training scenarios before training, simulator control by setting training conditions during training, and debriefing (evaluation by data storage / replay) after training. 1000); and

The drive control system 800,
Trainee motion control unit 810 for controlling the movement of the motion control line 500 to move the trainee's posture up and down / back and forth so that the trainee who escaped the emergency to feel the parachute descent situation, and
The trainee detects the pull when the parachute pulls the control line, and the control line sensor 820 provides a detection signal to the reaction force generator 820 and the simulation engine / image generating computer 900 when the pull is detected;
Reaction force generation unit 830 for generating a reaction force generated in the opposite direction to the pulling force when the trainee pulls the parachute control line when providing a detection signal from the control line sensor 830,
In order to provide an emergency escape effect to the trainees by moving the injection sliding part 220 of the emergency injection part 200 backwards on the injection guide groove 131 of the lower frame 130 when selecting the trainee's emergency escape. An injection driver 840,
In this case, the simulation engine / image generating computer 900 that receives the detection signal from the control line sensor 820, the image information that the drop situation (falling direction) is changed according to the strength of the trainee pulls the parachute control line 600 Aircraft pilot emergency escape training simulator system using a parachute, characterized in that to provide the HMD (300)
The method according to claim 1,
The frame unit 100,
One side is connected to the upper frame 120 to support the upper frame 120, the other side is a plurality of support frames 110 connected to the lower frame 130,
An upper frame 120 connected to the plurality of support frames 110 and having a drive control system 800 formed at one side thereof;
Emergency pilot training system for aircraft pilot using a parachute, characterized in that it comprises a lower frame 130 is connected to a plurality of support frame 110 and the injection guide groove 131 is formed.
The method according to claim 1,
The emergency injection unit 200,
It is formed in the same shape as the aircraft cockpit to provide a space for the trainees seated, the injection cockpit 210 for raising and lowering on the injection sliding part 220, to raise the seated trainees to a certain height,
Lifting and lowering guide grooves 221 for guiding the rising and falling of the injection cockpit 210 is formed, and trainees by moving backward sliding on the injection guide grooves 131 formed in the lower frame 130 when selecting the emergency escape of the trainees Emergency escape training simulator system using a parachute, characterized in that it comprises an injection sliding portion 220 for providing an emergency escape effect to the
The method according to claim 1,
The HMD 300 is,
Parachute-based aircraft pilot emergency escape training simulator system, characterized in that the trainee further comprises a gyro sensor interlocked to maintain the aerial aerial flight attitude
The method according to claim 1,
Aircraft pilot emergency escape training simulator system using a parachute, characterized in that it further comprises; a plurality of blowers 1100 for generating a wind for the trainee to enhance the emergency escape parachute drop experience effect
The method according to claim 1,
The simulation engine / image generation computer 900,
Simulation engine unit 910 for processing simulation conditions such as free fall of parachute and dynamic characteristic model of parachute, simulation model of environment such as wind, malfunction of parachute and providing control signal according to simulation situation to drive control system; ,
According to the processing situation of the simulation engine unit 910, image data consisting of three-dimensional object model, such as parachute, aircraft, character and terrain information is retrieved from the database unit 930 and rendered, and weekly to the rendered image data Trainees are able to wear the trainees by real-time 3D image information that changes according to the trainee's line of sight and parachute control by realizing various weather effects such as weather, snow, cloud, rain, and storm, and various predictable special effects. An image generator 920 provided to one HMD 300,
Simulator system for emergency pilot training using the parachute, characterized in that it comprises a database unit 930 for storing the modeling value and the image information generated by the simulation engine unit 910 and the image generation unit 920.
The method according to claim 1,
The instructor control unit 1000,
Provides the ability to create or load various training scenarios run by the trainees, edit the created or loaded training scenarios, and perform simulation training by the computer simulator before the trainees perform the actual training according to the training scenarios. The training results of the trainees are provided based on the trainee drop posture extraction data acquired through the motion sensor unit 700 during training and the trainees pull and manipulate the parachute control line 600 as the train time elapses. Instructor control computer 1010 that provides the ability to evaluate and analyze;
Allows the instructor to comprehensively and objectively understand the training status of the trainees while the instructor is watching the video information provided to the HMD 300, the video information on the 3D space where the trainees descend from the air, and the actual picture of the trainees photographed by the surrounding cameras. With instructor monitor 1020
Simulator system for emergency escape pilot using a parachute characterized in that it comprises an instructor microphone (1030) to explain the training situation to the trainees immersed in the virtual reality by the HMD (300), or to provide appropriate instructions or guidance.

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