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Pilot space situational awareness auxiliary training system

A situation awareness and training system technology, applied in the field of flight training, can solve the problems of no joystick and ineffective training, etc., and achieve the effect of clear turbulence state

Active Publication Date: 2020-02-07
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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  • Pilot space situational awareness auxiliary training system
  • Pilot space situational awareness auxiliary training system
  • Pilot space situational awareness auxiliary training system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0029] This embodiment provides a space situational awareness auxiliary training system for pilots, and implements the present invention through basic necessary technical features to solve the problems raised in the technical background section of this application document.

[0030] Specifically, such as Figure 1-3 As shown, the present invention provides a pilot space situational awareness auxiliary training system, including a spherical iron shell 1, a door is opened on the spherical iron shell 1, and a support column for supporting the spherical iron shell 1 is provided under the spherical iron shell 1 2. The bottom of the inner cavity of the spherical iron shell 1 is connected with a support platform 4 through a plurality of lifters 5, and the lifting end of each lifter 5 is movably connected with the bottom surface of the support platform 4, and the top of the support platform 4 An annular chute 6 is provided, and two sliding blocks 10 opposite to each other are slidably...

Embodiment 2

[0037] This example is based on Example 1 and optimizes the implementation in Example 1, so that this example is more stable and has better performance during operation, but it is not limited to the one described in this example implementation.

[0038] Specifically, the shape of the support platform 4 is triangular, the number of the lifters 5 is three, and each lifter 5 is connected to each corner of the bottom surface of the triangular support platform 4 .

[0039] Using the triangular shape as the shape of the support platform 4 can produce a three-dimensional effect when the support platform 4 is bumped, and more realistically restore the flight bumps of the aircraft.

[0040] In this embodiment, the lifter 5 is a scissor lifter, the lifting end of the scissor lifter is flexibly connected to the bottom surface of the support table 4, and the scissor lifter and the central processing signal connection, and the scissor lifter is electrically connected to the power supply d...

Embodiment 3

[0043] This example is based on Example 1 and optimizes the implementation in Example 1, so that this example is more stable and has better performance during operation, but it is not limited to the one described in this example implementation.

[0044] Specifically, the number of the sliding wheels 17 is one and is arranged in the center of the side of the moving block 12 facing the inner cavity, and the moving block 12 is provided with a plurality of evenly distributed and used for auxiliary sliding wheels on the side facing the inner cavity. 17 running stable support wheels 17.

[0045] In this embodiment, the moving block 12 runs more stably through the support wheel 17, and meanwhile, the material of the support wheel 179 is consistent with that of the sliding wheel 17, which is also the material of the magnet.

[0046] In this embodiment, the supporting wheels 17 include a plurality of connecting rods respectively fixed on the moving block 12, and the free end of each c...

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Abstract

The invention discloses a pilot space situational awareness auxiliary training system comprising a spherical iron shell; the bottom of the inner cavity of the spherical iron shell is connected with asupporting table through a plurality of lifting devices; an annular sliding chute is formed in the upper surface of the supporting table; two sliding blocks are connected to the annular sliding chutein a sliding fit mode; supporting rods are fixed to the sliding blocks; first motors are fixed on the opposite surfaces of the upper ends of the two supporting rods respectively; the output shafts ofthe first motors are connected to an aircraft simulation machine through connecting rods; first driving mechanisms are arranged at the bottoms of the sliding blocks; the inner cavity of the sphericaliron shell is provided a moving block; a sliding wheel driven by a second driving mechanism and made of a magnet is arranged on one side of the moving block; a sound playing source is arranged on theside, facing the aircraft simulation machine, of the moving block; and a gyroscope is further arranged on the moving block. According to the auxiliary training system in the invention, the jounce state of an aircraft is simulated during flight, and after the jounce state, a pilot needs to adjust the space state of the aircraft to the position of a sound source, wherein the sound source is at any position in the direction of the nose of the aircraft.

Description

technical field [0001] The invention relates to the technical field of flight training, in particular to a pilot space situational awareness auxiliary training system. Background technique [0002] Flight personnel are often faced with complex air situations, and maintaining good space situational awareness is very important to prevent human errors. Because the human spatial orientation system itself can cause ambiguity, such as the inability of otolithic organs to distinguish gravity and inertial forces, it leads to the illusion of body gravity. Therefore, in addition to the orientation perception system, it is meaningful to look for a clue to improve the ability of spatial attitude perception. [0003] When the pilot is flying, he often encounters some turbulence in the air. After the turbulence passes, the flight attitude of the aircraft will be inconsistent with the original flight attitude. At this time, the pilot must adjust the aircraft to normal in the flight attit...

Claims

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Application Information

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Patent Type & Authority Applications(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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