CN117437828B - Rotary cabin, training system and training method thereof - Google Patents

Rotary cabin, training system and training method thereof Download PDF

Info

Publication number
CN117437828B
CN117437828B CN202311754740.XA CN202311754740A CN117437828B CN 117437828 B CN117437828 B CN 117437828B CN 202311754740 A CN202311754740 A CN 202311754740A CN 117437828 B CN117437828 B CN 117437828B
Authority
CN
China
Prior art keywords
cabin
base
execution instruction
angle
motion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202311754740.XA
Other languages
Chinese (zh)
Other versions
CN117437828A (en
Inventor
包军权
艾正松
郭辉
裴佳法
蔡江宁
杜雪松
王春聚
李成送
刘涛
茅卫平
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Suzhou Hi Elec Equipment Co ltd
Original Assignee
Suzhou Hi Elec Equipment Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Suzhou Hi Elec Equipment Co ltd filed Critical Suzhou Hi Elec Equipment Co ltd
Priority to CN202311754740.XA priority Critical patent/CN117437828B/en
Publication of CN117437828A publication Critical patent/CN117437828A/en
Application granted granted Critical
Publication of CN117437828B publication Critical patent/CN117437828B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/085Special purpose teaching, e.g. alighting on water, aerial photography
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/46Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer the aircraft being a helicopter

Landscapes

  • 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)
  • Rehabilitation Tools (AREA)

Abstract

The application discloses rotatory cabin, training system and training method thereof relates to simulation training technical field for solve in the prior art aerial and take on a load analog device because the problem of total power is too high, the device includes: the base is connected with the base through a first rotating shaft, and a rotary support is arranged between the base and the base; a first servo motor is arranged on the base; the support posts are 2 in number and are symmetrically arranged on the base; the two ends of the outer frame are arranged on the two struts and are connected through two second rotating shafts, the second rotating shafts are connected with second servo motors, and the second servo motors are used for driving the outer frame to rotate; the cabin is connected with the first gear shaft through a first gear shaft, the second gear shaft is connected with the first gear shaft through a chain and is connected with the third servo motor. The three-degree-of-freedom rotation of the cabin is completed by arranging the base, the pillar outer frame and the cabin on the base, and the servo motor is arranged for transmission, and the rotary support is arranged to reduce friction and surface contact and provide rotary motion, so that the total power is reduced.

Description

Rotary cabin, training system and training method thereof
Technical Field
The invention relates to the technical field of simulation training, in particular to a rotary cabin, a training system and a training method thereof.
Background
The helicopter flight acceleration environment is required to be simulated in the air assault training, the anti-dizziness capability training and the aviation acceleration environment adaptability training under the three-degree-of-freedom rotation environment are carried out, and the easy vestibular illusion adaptability is improved by matching with a rotary seat.
There is a need for a new rotary cabin that reduces the total power used by the rotary cabin equipment and increases the load carrying capacity.
Disclosure of Invention
The purpose of the application is to provide a rotatory cabin, solves the problem that the total power that current rotatory cabin equipment used among the prior art is too high and bear inadequately.
In order to achieve the above purpose, the embodiment of the present application adopts the following technical scheme:
the base is arranged on the plane; the base is arranged on the base, a rotary support is arranged between the base and is used for being matched with a first servo motor, and the first servo motor drives the base to rotate; the support posts are 2 in number and symmetrically arranged at the edges of two sides of the base; the two ends of the outer frame are arranged on the two struts, one end of the outer frame is provided with a second servo motor which is used for driving the outer frame to rotate, and the other end of the outer frame is provided with a second rotating shaft which is connected with the struts; the cabin is arranged in the outer frame, one end of the cabin is provided with a first gear, a second gear, a chain and a third servo motor, the other end of the cabin is provided with a third rotating shaft connected with the outer frame, the cabin is internally provided with a mounting base, and the mounting base is parallel to the rotation axis of the cabin; the base, the frame and the cabin carry out independent rotary motion, and servo motor three is used for driving gear one, and gear one drives gear two to drive the cabin and rotate, servo motor two is used for driving the frame and rotates, and servo motor one is used for cooperating the gyration support to drive the base and rotate, carries out the multi-angle rotation that takes cabin swing and frame transverse put as the main.
Further, in the embodiment of the invention, a plurality of fixing plates are arranged at the bottom of the base, and mounting holes are arranged on the fixing plates and used for fixing the base on a plane.
Further, in the embodiment of the invention, a first rotary support plate is arranged at the top of the base, a first through hole is arranged in the middle of the first rotary support plate, and the outer sides of the first through holes are respectively provided with a plurality of threaded holes for being fixedly connected with a first support ring of the rotary support; the bottom of the base is provided with a second rotary support plate, the middle part of the first rotary support plate is provided with a second through hole, and the outer side of the second through hole is also provided with a plurality of through parts and a third through hole.
Further, in the embodiment of the invention, the cabin is formed by welding a plurality of round pipes.
The embodiment of the application also discloses rotatory cabin training system is applied to above-mentioned arbitrary rotatory cabin, including following module:
the receiving module I is used for receiving information I, the information I is obtained through terminal sending, and the information I comprises a movement angle I and a movement time I of the target device;
the receiving module II is used for receiving an execution instruction I, the execution instruction I is obtained through the transmission of the terminal, and the execution instruction I is used for starting the target device to enable the target device to reciprocate according to the movement angle information;
the first sending module is used for responding to the step of receiving the execution instruction and sending the execution instruction;
the receiving module III is used for receiving the first movement information, wherein the first movement information comprises physiological parameters and is obtained by sending through preset physiological equipment;
the receiving module IV is used for acquiring second motion information, wherein the second motion information comprises a second motion angle and a second motion time of the target device;
the first judging module is used for judging whether the parameter of the first motion information is outside a preset threshold value, if the parameter is in accordance with the preset threshold value, a second execution instruction is produced, and the second execution instruction is used for stopping the motion of the target device;
the judging module II is used for judging whether the parameter of the second movement time is within the threshold range of the first movement time, and if the parameter is in accordance with the threshold range of the first movement time, the preset condition is met, and an execution instruction II is generated;
and the receiving module II is used for receiving the execution instruction II, responding to the execution instruction II, enabling the servo motor I in the target device to control the rotation of the rolling angle of the bottom plate, enabling the rotating shaft and the servo motor II to control the pitching angle of the outer frame to rotate, and controlling the rotation of the heading angle of the cabin.
The embodiment of the application also discloses a rotary cabin training method which is applied to any rotary cabin and comprises the following steps:
receiving information I, wherein the information I is obtained by sending by a terminal and comprises a movement angle I and a movement time I of a target device;
receiving an execution instruction I, wherein the execution instruction I is obtained by sending through a terminal, and the execution instruction I is used for starting a target device to enable the target device to reciprocate according to the movement angle information;
responding to the step of receiving the execution instruction, and sending the execution instruction;
receiving motion information I, wherein the motion information I is obtained by sending through preset physiological equipment;
acquiring second motion information, wherein the second motion information comprises a second motion angle and a second motion time of the target device;
judging whether the parameter of the first motion information is outside a preset threshold value, if so, meeting a preset condition, and producing an execution instruction II which is used for stopping the motion of the target device;
judging whether the parameter of the second movement time is within the threshold range of the first movement time, if so, meeting the preset condition, and generating an execution instruction II;
and receiving an execution instruction II and responding to the execution instruction II.
The first motion angle comprises a look-up motion angle, a roll motion angle and a heading motion angle of the target device.
The motion angle two comprises a look-up angle, a roll angle and a heading angle of the target device.
The second step of obtaining the motion information further comprises the step of sending the motion information II, wherein the motion information II is used for enabling the terminal to receive and display the motion information II.
The second step of receiving the execution instruction comprises the step of obtaining the execution instruction II through a terminal, so that a first servo motor in the target device controls the rotation of the rolling angle of the bottom plate, a second servo motor and a rotating shaft control the rotation of the pitching angle of the outer frame, and the rotation of the heading angle of the cabin is controlled.
Further, in an embodiment of the present invention, the first motion angle includes a look-up motion angle, a roll motion angle, and a heading motion angle of the target device.
Further, in the embodiment of the present invention, the second movement angle includes a look-up angle, a roll angle and a heading angle of the target device.
Further, in the embodiment of the present invention, the step of obtaining the second motion information further includes sending the second motion information, so that the terminal receives and displays the second motion information.
Further, in the embodiment of the present invention, the step of receiving the second execution instruction includes obtaining the second execution instruction by the terminal.
The base is arranged on a horizontal plane for fixing, the base is arranged on the base, a rotary support is arranged between the base and the base to increase the load of the base, and the rotary support is matched with a servo motor to control the rotation of the rolling angle of the bottom plate; then, the two edges of the base are provided with the support posts, the outer frame is arranged on the support posts, and the pitching angle rotation of the outer frame is controlled by matching with the rotating shaft and the servo motor II; the outer frame is provided with a cabin, and the cabin is matched with a rotating shaft, a gear chain and a servo motor to control the rotation of the heading angle of the cabin; under the condition that the number of seats is 4, the power consumed by the system is calculated to be 408.6V, 4.9A of a machine current No. 1, 6.31A of a machine current No. 2, 6.43A of a machine current No. 3, 2002.14VA of a machine power No. 1, 2578.266VA of a machine power No. 2, 1627.298VA of a machine power No. 3 and 7207.704VA of total power by measuring the current and voltage values of a power supply when the system works normally; the timer is used for timing for 1min, the recording device is used for carrying out uniaxial rotation, the number of turns is 21 turns/min on an X axis, 23 turns/min on a Y axis and 19 turns/min on a Z axis, and three degrees of freedom of a rotation angle are checked visually to be +/-360 degrees, so that the cabin can be used by four people under the condition of ensuring the rotating speed, the single power is not more than 3kW, the total power is not more than 9kW, and the technical effect of reducing the total power used by the rotating cabin device is achieved.
Drawings
Fig. 1 is a schematic view of a rotary cabin according to the present invention.
Fig. 2 is a schematic view of a base structure of a rotary cabin according to the present invention.
Fig. 3 is a schematic view of a base structure of a rotary cabin according to the present invention.
Fig. 4 is a schematic view of a strut structure of a rotary cabin according to the present invention.
Fig. 5 is a schematic view of a cabin structure of a rotary cabin according to the present invention.
Detailed Description
In order to make the objects, technical solutions, and advantages of the present invention more apparent, the embodiments of the present invention will be further described in detail with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are some, but not all, embodiments of the present invention, are intended to be illustrative only and not limiting of the embodiments of the present invention, and that all other embodiments obtained by persons of ordinary skill in the art without making any inventive effort are within the scope of the present invention.
In the description of the present invention, it should be noted that the terms "center," "middle," "upper," "lower," "left," "right," "inner," "outer," "top," "bottom," "side," "vertical," "horizontal," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate description of the present invention and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "a," an, "" the first, "" the second, "" the third, "" the fourth, "" the fifth, "and the sixth" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
For purposes of brevity and description, the principles of the embodiments are described primarily by reference to examples. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the embodiments. It will be apparent, however, to one of ordinary skill in the art that the embodiments may be practiced without limitation to these specific details. In some instances, well-known methods and structures have not been described in detail so as not to unnecessarily obscure the embodiments. In addition, all embodiments may be used in combination with each other.
Example 1
As shown in fig. 1, the device for cleaning the filtering device based on the filtering completion comprises:
a base 1, the base 1 being disposed on a plane; the base 2 is arranged on the base 1, the base 1 is connected with the base 2 through a first rotating shaft, and a rotary support is arranged between the base 1 and the base 2; the base 2 is provided with a first servo motor which is used for driving the base 2 to rotate by driving the rotating shaft; the support posts 3 are 2 in number and symmetrically arranged at two sides of the base 2; the two ends of the outer frame 4 are arranged on the two support posts 3 and are connected through two second rotating shafts, the second rotating shafts are connected with second servo motors, and the second servo motors are used for driving the outer frame 4 to rotate; cabin 5, cabin 5 inside is provided with mounting base 1, mounting base 1 is used for installing the seat, cabin 5's both ends are provided with reinforcing plate one 501 and reinforcing plate two 502, reinforcing plate one 501 sets up on frame 4 one inboard, reinforcing plate one 501 connects frame 4 one inboard through pivot three, cabin 5's another reinforcing plate one 501 sets up at frame 4 another inboard, through gear shaft one connection, still be provided with a gear shaft two on cabin 5's another reinforcing plate one 501, gear shaft two passes through the chain and is connected with gear shaft one, gear shaft connection servo motor three, servo motor three is used for driving cabin 5 rotation.
The device is characterized in that the base 1 and the base 2 are arranged separately, a rotary support is arranged between the base 1 and the base 2, the rotation is ensured to be carried out stably while the rotation load is borne, wherein the base 1 is arranged on a horizontal plane for fixing, the base 2 is arranged on the base 1, the rotary support is arranged between the base 2 and the base 1 to increase the load of the base 2, and the rotary support is matched with a servo motor to control the rotation of the roll angle of the bottom plate 301; then, the two sides of the base 2 are provided with the support posts 3, the outer frame 4 is arranged on the support posts 3, and the pitching angle rotation of the outer frame 4 is controlled by matching with the rotating shaft and the servo motor II; and set up cabin 5 on frame 4, the rotation of the course angle of cooperation pivot, gear chain and servo motor three control cabin 5 carries out the rotation training that takes reciprocating swing as the main part, reduces the demand to the whole bearing of trainer.
Specifically, as shown in fig. 2, a plurality of first fixing plates 101 are arranged at the bottom of the base 1, and are used for fixing the base 1 on a horizontal plane, the base 1 comprises a first frame 102 and a first support frame 103, the first frame 4 and the first support frame 103 are formed by welding and assembling a plurality of hollow square tubes, and a plurality of circular holes are formed in the square tubes, so that the lead threading and the servo motor can be conveniently fixed; the top of the base 1 is also provided with a first rotary support plate 104, the appearance of the first rotary support plate 104 is larger than the size of a gap reserved in the middle of the support frame, the middle of the first rotary support plate 104 is provided with a first through hole, and the outer sides of the first through holes are respectively provided with a plurality of threaded holes for being fixedly connected with a first support ring of the rotary support;
specifically, as shown in fig. 3, the base 2 comprises a second frame 203 and a second support frame 201, the second frame 4 and the second support frame 201 are formed by welding and assembling a plurality of hollow square tubes, the bearing capacity of the base 2 is increased, and a plurality of circular holes are formed in the square tubes so as to be convenient for fixing a lead threading tube and a servo motor;
specifically, the bottom of the base 2 is provided with a second slewing support plate 204, the middle of the second slewing support plate is provided with a second through hole, the outer side of the second through hole is also provided with a plurality of through parts and a third through hole for installing a plurality of slewing supports, wherein the second through hole is used for enabling the servo motor to drive the slewing support to drive the base 2 to rotate within a specified range once the servo motor drives the slewing support, and preferably, the number of the slewing support sleeves is set to 3, so that the rotation speed of the base 2 can reach 19 revolutions per minute and reach the required rotation speed of a Z axis.
Specifically, the upper end face and the lower end face of the second outer frame 4 are provided with a plurality of mounting holes, and the inner side of the outer frame 4 is symmetrically provided with connecting sheets for fixedly mounting the shell of the base 2; the two ends of the second support frame 201 are fixedly welded with the first connecting plate 202, and the first connecting plate 202 is positioned at the edges of the two sections of the second support frame 201.
Specifically, as shown in fig. 4, the strut 3 comprises a bottom plate 301, a column 302 and a second connecting plate 303, wherein a mounting hole is formed in the bottom plate 301 for mounting and positioning the first connecting plate 202, and a plurality of mounting grooves are formed in the bottom plate 301 for fixedly mounting the first connecting plate; wherein the number of the upright posts 302 is 2, the upright posts 302 are symmetrically arranged at the edge of the bottom plate 301, a gap is reserved between the two upright posts 302 by arranging a support column 305 for installing a second connecting plate 303, the second connecting plate 303 is positioned at the edge of the gap facing to the first rotary support plate 104, and a sufficient gap is reserved on the other surface for accommodating a rotating shaft and a second servo motor; wherein a reinforcing plate 304 is further provided between the base plate 301 and the upright 302 for increasing the load bearing of the column 3.
Specifically, as shown in fig. 5, the outer frame 4 includes a second frame 401, a frame connecting block and a third connecting plate 402, wherein the third frame is composed of a plurality of hollow rectangular steel pipes, the frame connecting block is used for connecting the plurality of frames three to form the outer frame 4 in cooperation with the third connecting plate 402, compared with the existing integral outer frame 4, the outer frame 4 is connected and supported through the frame 4 connecting block, the third connecting plate 402 is further fixedly connected on the upper end surface and the lower end surface of the frame connecting block, and the transverse bearing load of the outer frame 4 is enhanced in cooperation with the transverse bearing angle rotation of the outer frame 4, so that the outer frame 4 has enough bearing to support the bearing angle rotation of the cabin 5 of four people when the weight of the outer frame 4 is reduced; the third plate 402 is further provided with a frame connection means 403, such as a connection portion 404, which is provided with a connection hole.
Specifically, two ends of the outer side of the outer frame 4 are symmetrically provided with four connecting plates 405, the four connecting plates 405 are used for installing a rotating shaft to enable the outer frame 4 to rotate around the rotating shaft, gaps are reserved between the four connecting plates 405 and the support posts 3, and corresponding upright posts 302 are provided with fixing plates for clamping the second servo motor to drive the outer frame 4 to rotate.
Specifically, the cabin 5 is composed of a plurality of hollow round tubes, and a receiving portion is formed in the middle, and a seat support 503 is provided on the receiving portion for mounting and fixing a seat.
The base 1 is arranged on a horizontal plane for fixing, the base 2 is arranged on the base 1, a rotary support is arranged between the base 2 and the base 1 to increase the load of the base 2, and the rotary support is matched with a servo motor to control the rotation of the roll angle of the bottom plate 301; then, the two sides of the base 2 are provided with the support posts 3, the outer frame 4 is arranged on the support posts 3, and the pitching angle rotation of the outer frame 4 is controlled by matching with the rotating shaft and the servo motor II; the cabin 5 is arranged on the outer frame 4, and the rotation of the heading angle of the cabin 5 is controlled by matching with a rotating shaft, a gear chain and a servo motor; under the condition that the number of seats is 4, the power consumed by the system is calculated to be 408.6V, 4.9A of a machine current No. 1, 6.31A of a machine current No. 2, 6.43A of a machine current No. 3, 2002.14VA of a machine power No. 1, 2578.266VA of a machine power No. 2, 1627.298VA of a machine power No. 3 and 7207.704VA of total power by measuring the current and voltage values of a power supply when the system works normally; the timer is used for timing for 1min, the recording device is used for carrying out single-axis rotation, the number of turns is 21 turns/min, the Y axis is 23 turns/min, the Z axis is 19 turns/min, and three degrees of freedom of a rotation angle are checked visually to be +/-360 degrees, the cabin 5 can be used by four people under the condition of guaranteeing the rotation speed, the single power is not more than 3kW, the total power is not more than 9kW, the technical effect of reducing the total power used by the rotating cabin device is achieved, sub-training items of a pre-court training item are carried out, the dizziness resistance capability and the aviation acceleration environment adaptability of a plurality of people can be carried out, the training cost is reduced, the personnel post adaptability is used for assisting in selecting and pulling, students are familiar with knowing the aerial characteristics of the helicopter carrying environment in an analog environment in advance, and the helicopter real-time training expense is saved.
Example 2
In this embodiment, there is also provided a rotary cabin training system applied to the above rotary cabin to complete training, including the following devices:
the receiving module I is used for receiving information I, the information I is obtained through terminal sending, and the information I comprises a movement angle I and a movement time I of the target device; the receiving module II is used for receiving an execution instruction I, the execution instruction I is obtained through the transmission of the terminal, and the execution instruction I is used for starting the target device to enable the target device to reciprocate according to the movement angle information; the first sending module is used for responding to the step of receiving the execution instruction and sending the execution instruction; a receiving module III, which is used for receiving the first movement information, wherein the first movement information is obtained by sending through a preset physiological device; the receiving module IV is used for acquiring second motion information, wherein the second motion information comprises a second motion angle and a second motion time of the target device; the first judging module is used for judging whether the parameter of the first motion information is outside a preset threshold value, if the parameter is in accordance with the preset threshold value, a second execution instruction is produced, and the second execution instruction is used for stopping the motion of the target device; the judging module II is used for judging whether the parameter of the second movement time is within the threshold range of the first movement time, and if the parameter is in accordance with the threshold range of the first movement time, the preset condition is met, and an execution instruction II is generated; and the receiving module II is used for receiving the execution instruction II, responding to the execution instruction II, enabling the servo motor I in the target device to control the rotation of the rolling angle of the bottom plate, enabling the rotating shaft and the servo motor II to control the pitching angle of the outer frame to rotate, and controlling the rotation of the heading angle of the cabin.
Example 3
In this embodiment, there is also provided a training method for a rotary cabin, which is applied to the above rotary cabin to complete training, including the following steps:
receiving information I, wherein the information I is obtained by sending by a terminal and comprises a movement angle I and a movement time I of a target device;
receiving an execution instruction I, wherein the execution instruction I is obtained by sending through a terminal, and the execution instruction I is used for starting a target device to enable the target device to reciprocate according to the movement angle information;
responding to the step of receiving the execution instruction, and sending the execution instruction;
receiving motion information I, wherein the motion information I comprises physiological parameters and is obtained through transmission of preset physiological equipment;
acquiring second motion information, wherein the second motion information comprises a second motion angle and a second motion time of the target device;
judging whether the parameter of the first motion information is outside a preset threshold value, if so, meeting a preset condition, and producing an execution instruction II which is used for stopping the motion of the target device;
judging whether the parameter of the second movement time is within the threshold range of the first movement time, if so, meeting the preset condition, and generating an execution instruction II;
and receiving an execution instruction II, responding to the execution instruction II, enabling a servo motor I in the target device to control the rotation of the roll angle of the bottom plate, enabling a rotating shaft and the servo motor II to control the pitching angle of the outer frame to rotate, and controlling the rotation of the heading angle of the cabin.
Specifically, the first motion angle includes a look-up motion angle, a roll motion angle, and a heading motion angle of the target device.
Specifically, the second movement angle includes a look-up angle, a roll angle and a heading angle of the target device.
Specifically, the step of obtaining the second motion information further includes sending the second motion information, which is used for enabling the terminal to receive and display the second motion information.
Specifically, the step of receiving the second execution instruction includes obtaining the second execution instruction through the terminal.
The training platform comprises a rotary cabin, a touch screen control console, a motor control cabinet, a mounting base 1, a peripheral safety guardrail and a safety operation rule hanging chart. The main supporting software is 'three-degree-of-freedom rotating system preprogrammed control software', and the system software can preprogramme and control motor movement according to training subjects or subjects. When the physiological device is used for monitoring the physiological state of a user, in the physiological parameter module, four seats are corresponding, and physiological parameter data of each seat comprises heart rate, blood pressure/high pressure and blood pressure/low pressure data. After binding the device, heart rate data etc. will change and an electrocardiographic curve will be generated and after the training has started, these data will be recorded.
While the foregoing has been described in terms of illustrative embodiments thereof, so that those skilled in the art may appreciate the present application, it is not intended to be limited to the precise embodiments so that others skilled in the art may readily utilize the present application to its various modifications and variations which are within the spirit and scope of the present application as defined and determined by the appended claims.

Claims (9)

1. A rotary cabin, comprising:
the base is arranged on a plane;
the base is arranged on the base, a rotary support is arranged between the base and is used for being matched with a first servo motor, and the first servo motor drives the base to rotate;
the number of the struts is 2, and the struts are symmetrically arranged at the edges of two sides of the base;
the two ends of the outer frame are arranged on the two support posts, one end of the outer frame is provided with a second servo motor which is used for driving the outer frame to rotate, and the other end of the outer frame is provided with a second rotating shaft which is connected with the support posts;
the cabin is arranged in the outer frame, one end of the cabin is provided with a first gear, a second gear, a chain and a third servo motor, the other end of the cabin is provided with a third rotating shaft connected with the outer frame, the cabin is internally provided with a mounting base, and the mounting base is parallel to the rotation axis of the cabin;
the base, the outer frame and the cabin perform independent rotary motion, the servo motor III is used for driving the gear I, the gear I drives the gear II so as to drive the cabin to rotate, the servo motor II is used for driving the outer frame to rotate, and the servo motor I is used for driving the base to rotate by being matched with a rotary support so as to perform multi-angle rotation mainly comprising cabin swing and outer frame transverse arrangement;
the rotary cabin further comprises a rotary cabin training system comprising:
the receiving module I is used for receiving information I, wherein the information I is obtained by sending a terminal, and the information I comprises a movement angle I and a movement time I of a target device;
the receiving module II is used for receiving an execution instruction I, the execution instruction I is obtained by sending the execution instruction I through the terminal, and the execution instruction I is used for starting the target device to enable the target device to reciprocate according to the movement angle information;
the first sending module is used for responding to the second receiving module and sending the first executing instruction;
a receiving module III, configured to receive exercise information I, where the exercise information I includes physiological parameters, and the exercise information I is obtained by sending through a predetermined physiological device;
a receiving module IV, configured to obtain motion information II, where the motion information II includes a motion angle II and a motion time II of the target device;
the first judgment module is used for judging whether the parameter of the first motion information is outside a preset threshold value, if yes, a preset condition is met, and an execution instruction II is generated, wherein the execution instruction II is used for stopping the motion of the target device;
the judging module II is used for judging whether the parameter of the second movement time is within the threshold range of the first movement time, and if the parameter is in accordance with the threshold range of the first movement time, the preset condition is met, and the second execution instruction is generated;
and the receiving module V is used for receiving the execution instruction II and responding to the execution instruction II, so that the first servo motor in the target device controls the rotation of the roll angle of the bottom plate, the rotating shaft and the second servo motor control the pitching angle of the outer frame to rotate, and the heading angle of the cabin to rotate.
2. A rotary cabin according to claim 1, characterized in that the base bottom is provided with a number of fixing plates, which are provided with mounting holes for fixing the base on a plane.
3. The rotary cabin according to claim 1, wherein the top of the base is provided with a first slewing support plate, the middle of the first slewing support plate is provided with a first through hole, and a plurality of threaded holes are uniformly distributed on the outer side of the first slewing support plate and are used for being fixedly connected with a first supporting ring of the slewing support; the base bottom is provided with the gyration backup pad II, gyration backup pad I middle part is provided with the through-hole II, the through-hole II outside still is provided with a plurality of through-parts and a through-hole III.
4. A rotary cabin according to claim 1, characterized in that the cabin consists of several round tube welds.
5. A method of rotary cabin training for a rotary cabin according to claim 1, comprising:
receiving information I, wherein the information I is obtained by sending by a terminal, and the information I comprises a movement angle I and a movement time I of a target device;
receiving an execution instruction I, wherein the execution instruction I is obtained by sending through the terminal, and the execution instruction I is used for starting the target device to enable the target device to reciprocate according to the movement angle information;
a step of responding to the received execution instruction I, and sending the execution instruction I;
receiving exercise information I, wherein the exercise information I is obtained through transmission of preset physiological equipment;
acquiring motion information II, wherein the motion information II comprises a motion angle II and a motion time II of the target device;
judging whether the parameter of the first motion information is outside a preset threshold value, if so, meeting a preset condition, and generating an execution instruction II, wherein the execution instruction II is used for stopping the motion of the target device;
judging whether the parameter of the second movement time is within the threshold range of the first movement time, if so, meeting the preset condition, and generating the second execution instruction;
and receiving the second execution instruction, responding to the second execution instruction, enabling a first servo motor in the target device to control the rotation of the roll angle of the bottom plate, enabling a rotating shaft and the second servo motor to control the pitching angle of the outer frame to rotate, and controlling the rotation of the heading angle of the cabin.
6. The rotary cabin training method of claim 5 wherein the first motion angle comprises a look-up motion angle, a roll motion angle, and a heading motion angle of the target device.
7. The rotary cabin training method of claim 5 wherein the second motion angle comprises a look-up angle, a roll angle, and a heading angle of the target device.
8. The method of claim 5, wherein the step of obtaining the second motion information further comprises sending the second motion information to enable the terminal to receive and display the second motion information.
9. A method of training a rotary cabin according to claim 5, wherein the step of receiving the second execution instruction comprises obtaining the second execution instruction by the terminal.
CN202311754740.XA 2023-12-20 2023-12-20 Rotary cabin, training system and training method thereof Active CN117437828B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202311754740.XA CN117437828B (en) 2023-12-20 2023-12-20 Rotary cabin, training system and training method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202311754740.XA CN117437828B (en) 2023-12-20 2023-12-20 Rotary cabin, training system and training method thereof

Publications (2)

Publication Number Publication Date
CN117437828A CN117437828A (en) 2024-01-23
CN117437828B true CN117437828B (en) 2024-03-29

Family

ID=89551989

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202311754740.XA Active CN117437828B (en) 2023-12-20 2023-12-20 Rotary cabin, training system and training method thereof

Country Status (1)

Country Link
CN (1) CN117437828B (en)

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2003204243A1 (en) * 2002-09-06 2004-03-25 Barask Paraskevopoulos Motion simulator
CN104637364A (en) * 2015-01-28 2015-05-20 北京蓝天航空科技有限责任公司 Rotating flight simulator
CN206097572U (en) * 2016-08-03 2017-04-12 北京蓝天航空科技股份有限公司 Flight simulator of triaxial qxcomm technology
CN206672418U (en) * 2017-03-29 2017-11-24 四川龙睿三航科技有限公司 A kind of rotary simulation system of Three Degree Of Freedom
CN110930812A (en) * 2019-10-18 2020-03-27 深圳威阿科技有限公司 Control system for airplane simulation cockpit
CN212208630U (en) * 2020-04-28 2020-12-22 深圳威阿科技有限公司 Flight training simulation system
CN112735223A (en) * 2020-12-22 2021-04-30 中国人民解放军空军预警学院 Flight simulation training device
CN213781279U (en) * 2020-11-25 2021-07-23 青岛蓝天航空科技有限公司 Triaxial omnidirectional simulator control system
CN113409648A (en) * 2021-06-17 2021-09-17 中国人民解放军空军特色医学中心 Flight pitching illusion simulation method and device and flight illusion simulator
CN116884288A (en) * 2023-06-20 2023-10-13 安徽星戎科技有限公司 Dizziness-resistant training platform and method

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2003204243A1 (en) * 2002-09-06 2004-03-25 Barask Paraskevopoulos Motion simulator
CN104637364A (en) * 2015-01-28 2015-05-20 北京蓝天航空科技有限责任公司 Rotating flight simulator
CN206097572U (en) * 2016-08-03 2017-04-12 北京蓝天航空科技股份有限公司 Flight simulator of triaxial qxcomm technology
CN206672418U (en) * 2017-03-29 2017-11-24 四川龙睿三航科技有限公司 A kind of rotary simulation system of Three Degree Of Freedom
CN110930812A (en) * 2019-10-18 2020-03-27 深圳威阿科技有限公司 Control system for airplane simulation cockpit
CN212208630U (en) * 2020-04-28 2020-12-22 深圳威阿科技有限公司 Flight training simulation system
CN213781279U (en) * 2020-11-25 2021-07-23 青岛蓝天航空科技有限公司 Triaxial omnidirectional simulator control system
CN112735223A (en) * 2020-12-22 2021-04-30 中国人民解放军空军预警学院 Flight simulation training device
CN113409648A (en) * 2021-06-17 2021-09-17 中国人民解放军空军特色医学中心 Flight pitching illusion simulation method and device and flight illusion simulator
CN116884288A (en) * 2023-06-20 2023-10-13 安徽星戎科技有限公司 Dizziness-resistant training platform and method

Also Published As

Publication number Publication date
CN117437828A (en) 2024-01-23

Similar Documents

Publication Publication Date Title
CN102975783B (en) Single-wheel type pipe climbing robot outside pipes
JP2014528868A (en) 2-axis mount for use in small unmanned aerial vehicles and 3-axis mount for use in small unmanned aerial vehicles
CN117437828B (en) Rotary cabin, training system and training method thereof
CN207397535U (en) Illusion simulator motion platform
CN213789806U (en) A lower waist trainer for dance teaching
CN219551835U (en) Shock-resistant hanging bracket test device
CN210933767U (en) Novel sky wheel cabin suspended structure
CN210804848U (en) Aircraft teaching model passenger cabin
CN213450211U (en) Aerial ladder with adjustable fire control is used
CN204106979U (en) A kind of novel climbing mast ladder
CN212782369U (en) Driving simulator
CN107128402A (en) A kind of new omnidirectional may move photographic car
CN214623089U (en) Device for monitoring wind energy gradient
CN219963369U (en) Vestibule function trainer
CN210219150U (en) Angle-adjustable dome screen
CN214744766U (en) New energy automobile battery AC-DC converter teaching platform
CN216721474U (en) All-round support and use its AI safety in production supervision device
CN216287468U (en) A time limit for a project progress display device for building engineering project management
CN214428304U (en) Mobile display device for psychological education
CN212724404U (en) Science popularization type astronaut blood distribution simulation training device
CN213131891U (en) Driving gear disengaging gear of rotary car
CN218295001U (en) LED intelligent display practical training resource management device
CN216243020U (en) Multi freedom cloud platform structure of camera
CN215982006U (en) High-efficient type suspension type hydrogenation machine
CN214700118U (en) Track traffic engineering site operation safety control device

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant