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A Pilot Spatial Situational Awareness Auxiliary Training System

A situational awareness and training system technology, applied in the field of flight training, can solve the problems of no joystick and ineffective training

Active Publication Date: 2021-08-20
FOURTH MILITARY MEDICAL UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the current training of this skill for pilots, it is usually practiced by drawing the scene outside the aircraft window for the pilot to judge. However, this method does not have an actual joystick, which is quite different from the actual operation and cannot be effective. to train

Method used

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  • A Pilot Spatial Situational Awareness Auxiliary Training System
  • A Pilot Spatial Situational Awareness Auxiliary Training System
  • A Pilot Spatial Situational Awareness Auxiliary Training System

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0029] This embodiment provides a pilot spatial informational auxiliary training system to implement the present invention by basic necessity, to solve the problems raised by the technical background section in the present application.

[0030] Specifically, such as Figure 1-3 As shown, the present invention provides a pilot spatial manner aware auxiliary training system, including a spherical iron shell 1, a door, a spherical iron shell 1 having a support column for supporting a spherical iron shell 1 2, the bottom portion of the spherical iron shell 1 is connected to a support table 4 through a plurality of lift 5, and the elevator end of each of the lifter 5 is connected to the bottom surface of the support table 4, the support table 4 The annular chute 6 is opened, and the ring slide 6 is slidably coupled to the slider 10 having two positions, and the longitudinal support rod 7 is fixed to the slider 10, and the upper surfaces of the upper ends of the two support rods are fixe...

Embodiment 2

[0037] This embodiment is based on Embodiment 1 and optimizes the embodiments in Example 1 such that the present embodiment is more stable in operation, more performance is more good, but is not limited to the one described in this example. Embodiment.

[0038] Specifically, the shape of the support table 4 is a triangular shape, and the number of the lift 5 has three, and each of the elevator 5 is connected to each of the top corners of the bottom surface of the triangular support table 4, respectively.

[0039] The shape of the triangular shape is used as the shape of the support table 4, and when the support table 4 is bumpy, the three-dimensional effect can be generated, and the flight bump of the aircraft can be generated.

[0040] In the present embodiment, the riser 5 is a shear-type lifter, a raised end activity of the shear-type lifter to be attached to the bottom surface of the support table 4, the shear-type lifter and the central processing. The signal connection is el...

Embodiment 3

[0043] This embodiment is based on Embodiment 1 and optimizes the embodiments in Example 1 such that the present embodiment is more stable in operation, more performance is more good, but is not limited to the one described in this example. Embodiment.

[0044] Specifically, the number of the slide wheel 17 has one and is provided in the center of the moving block 12 facing the inner chamber side, and the moving block 12 is provided with a plurality of uniform distributions on one side of the inner chamber and used to assist the slide wheel. 17 Operate a stable support wheel 16.

[0045] In the present embodiment, by the support wheel 16, the moving block 12 operates more stable, and the material of the support wheel 16 is consistent with the material of the slider 17, and is also the material of the magnet.

[0046] In the present embodiment, the support wheel 16 includes a plurality of connecting rods that are respectively fixed to the moving block 12, and the free end of each c...

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Abstract

The invention discloses a space situation awareness auxiliary training system for pilots, which comprises a spherical iron shell. The bottom of the inner cavity of the spherical iron shell is connected with a support platform through a plurality of lifters, and an annular chute is provided on the support platform. There are two sliding blocks connected by sliding fit, and support rods are fixed on the sliding blocks. First motors are respectively fixed on the opposite surfaces of the upper ends of the two support rods. The connecting rod of the output shaft of the first motor is connected to the aircraft simulator. The bottom is provided with a first driving mechanism, the inner cavity of the spherical iron shell is provided with a moving block, one side of the moving block is provided with a sliding wheel driven by the second driving mechanism and made of a magnet, and the side of the moving block facing the aircraft simulator is provided There is a sound playback source, and a gyroscope is also provided on the moving block. The invention simulates the turbulent state of the aircraft during flight, and after the turbulent state, the pilot needs to adjust the spatial state of the aircraft to the position of the sound source, wherein the sound source is at any position in the direction of the nose of the aircraft.

Description

Technical field [0001] The present invention relates to the field of flight training, and in particular, to a pilot spatial situation aware auxiliary training system. Background technique [0002] Flights often face complex empty situations, while maintaining a good spatial situation perceived ability is important for preventing people. Since the human space orientation system itself can cause ambiguity, such as the ear strainer cannot distinguish between gravity and inertial force, the body gravity is caused. Therefore, in the direction of the directional perception system, it makes sense to find a lead in improving space attitude perception. [0003] When the pilot is in flight, it will often encounter some bumps in the air. After the bumpy state, it will lead to inconsistent the flight attitude of the aircraft and the original flying attitude. At this time, the pilot will adjust the aircraft to normal. Flight posture. [0004] For the above case, the pilot should conduct frequ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G09B9/08G09B9/10G09B9/20
CPCG09B9/08G09B9/10G09B9/20
Inventor 程珊胡文东孙继成马进张太辉熊凯文
Owner FOURTH MILITARY MEDICAL UNIVERSITY
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