CN113947969A - Flight special situation disposal experience system and operation method - Google Patents
Flight special situation disposal experience system and operation method Download PDFInfo
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- CN113947969A CN113947969A CN202010683430.3A CN202010683430A CN113947969A CN 113947969 A CN113947969 A CN 113947969A CN 202010683430 A CN202010683430 A CN 202010683430A CN 113947969 A CN113947969 A CN 113947969A
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- 238000000034 method Methods 0.000 title claims abstract description 25
- 230000008447 perception Effects 0.000 claims abstract description 8
- 230000009471 action Effects 0.000 claims description 10
- 230000000694 effects Effects 0.000 claims description 10
- 230000008859 change Effects 0.000 claims description 5
- 230000000704 physical effect Effects 0.000 claims description 3
- 230000008569 process Effects 0.000 abstract description 9
- 230000002457 bidirectional effect Effects 0.000 abstract description 6
- 238000006243 chemical reaction Methods 0.000 abstract description 2
- 238000004088 simulation Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- 238000005461 lubrication Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 230000001960 triggered effect Effects 0.000 description 2
- 206010000369 Accident Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/30—Simulation of view from aircraft
- G09B9/307—Simulation of view from aircraft by helmet-mounted projector or display
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- 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)
- User Interface Of Digital Computer (AREA)
Abstract
The invention discloses a flight special situation disposal experience system and an operation method, and relates to the technical field of flight special situation experience, wherein the flight special situation disposal experience system comprises a pedal group, a data glove, a head display device, a base station and a PC (personal computer) host, wherein the output ends of the data glove and the pedal group are electrically connected with the input end of the PC host, the PC host is in bidirectional connection with the head display device, and the head display device is respectively in bidirectional connection with a capture positioner and a perception positioner; an inner hexagonal wrench is placed at one side position of the pedal group, brake shafts are fixedly mounted on two sides of the upper end face of the pedal group, and a heel back cushion is fixedly mounted at a position, close to the lower end, of the inclined plane of each brake shaft. The system and the operation method can obtain better real data, so that an external operator can conveniently arrange the data, better experience numerical values can be obtained, the reaction capability and various strain capabilities of the airplane driver can be tested, and the airplane driver can conveniently operate and process the airplane.
Description
Technical Field
The invention relates to the technical field of special flight experience, in particular to a special flight handling experience system and an operation method.
Background
The airplane is an airplane which has one or more engines, generates forward thrust or pull force, generates lift force by fixed wings of a fuselage, flies in the atmosphere and is heavier than air, is one of the most important inventions in the beginning of the 20 th century, is increasingly an indispensable tool in modern civilization since the invention of the airplane, profoundly changes and influences the life of people, and opens up the history of conquering blue sky by people.
The aircraft is in the use, multiple unexpected condition can appear, driver and crew just when the operation, just equally can meet multiple problem, handle unexpected condition for driver and crew is better, just need to adopt a specified flight special situation to handle experience system and carry out experimental simulation to driver and crew and handle, be convenient for test response ability and multiple strain capacity to the aircraft crew, the aircraft crew of being convenient for operates the processing to the aircraft, thereby avoid the emergence of driving in-process accident.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a flight special situation handling experience system and an operation method, which solve the problems that various accident situations are easy to occur in the flight process of an airplane, drivers and passengers can also encounter various problems during operation, and a designated flight special situation handling experience system is required to be adopted to carry out test simulation processing on the drivers and passengers in order to better handle the accident situations.
In order to achieve the purpose, the invention is realized by the following technical scheme: a flight special situation handling experience system and an operation method thereof comprise a pedal group, a data glove, a head display device, a base station and a PC host, wherein the output ends of the data glove and the pedal group are electrically connected with the input end of the PC host, the PC host is in bidirectional connection with the head display device, the head display device is respectively in bidirectional connection with a capture positioner and a perception positioner, and the capture positioner and the perception positioner are both laser positioners;
the utility model discloses a USB adapter, including footboard group, heel, RJ12 male joint, RJ12 male joint one side electric connection has the USB adapter, USB adapter up end fixed mounting has the LED display, surface fixed mounting has RJ12 female joint on one side of the USB adapter, the terminal surface is close to lower extreme position department fixed mounting before the USB adapter has the selector switch near lower extreme intermediate position department fixed mounting, USB adapter one end position department electric connection has the USB joint.
Preferably, the finger positions on the outer surface of the data glove are fixedly provided with a plurality of sensors, and data lines are fixedly connected among the sensors.
Preferably, the head display device comprises an operating handle and an output device, and the operating handle and the output device are both in wireless connection with the head display device.
Preferably, terminal surface intermediate position department fixed mounting has a front panel before the basic station, terminal surface position department fixed mounting has a status indicator lamp in front panel upper end intermediate position before the basic station, terminal surface position department fixed mounting has a channel indicator lamp in front panel one side angular position before the basic station, the terminal surface is close to one side position department fixed mounting has the channel button in the middle of the lower extreme behind the basic station, the terminal surface is close to the middle opposite side position department fixed mounting of lower extreme behind the basic station has the data line port, terminal surface one side angular position department fixed mounting has the power source port behind the basic station, terminal surface opposite side corner position department fixed mounting has the USB port behind the basic station.
Preferably, the status indicator light and the channel indicator light are electrically connected with an external power supply and an external switch, and external connecting wires are arranged inside the data line port, the power supply port and the USB port.
Preferably, the annular outer surface of the operating handle is wrapped with a rubber pad, and the annular outer surface of the rubber pad is provided with anti-skid grains.
Preferably, the male connector of the RJ12 corresponds to the female connector of the RJ12, and the allen key is of a hexagonal structure.
Preferably, the flight special treatment experience system comprises the following steps:
step one, building an airplane three-dimensional model according to a proportion, and building a runway and an airport scene;
mounting each component in the engine on an airplane model to enable the airplane to have a real physical effect;
thirdly, the data glove acquires hand skeleton information through a sensor and transmits the hand skeleton information to an application program, the application program further calculates skeleton data, then assigns the data to corresponding skeletons, and the hand skeleton is driven to move through an IK algorithm;
triggering specific gestures according to different actions of the hand, completing the control of the operating handle and the triggering of the virtual keys, and achieving the effect of really controlling the airplane;
step five, the pedal group is stepped by feet to lead the pedals to change the angle and slide up and down, and the speed and the angle of the airplane are controlled;
step six, finishing a series of operations such as taking off, flying, landing and the like of the airplane by combining the step 4 and the step 5;
and seventhly, simulating and disposing the special flight situation by combining the sound and the special effect and changing the flight state.
Advantageous effects
The invention provides a special flight condition disposal experience system and an operation method. Compared with the prior art, the method has the following beneficial effects:
1. the flight special situation handling experience system and the operation method thereof realize the simulation of the actions of the airplane, including a flap, an empennage, an undercarriage and a speed reduction plate; manufacturing real flight effect air resistance and lift force according to an aerodynamic simulation flight physical system; simulating a real physical system to realize engine thrust and airplane gravity; acquiring and displaying the current power attribute of the airplane; the hand skeleton information is acquired through the sensor and transmitted to the application program, the application program further calculates skeleton data, then the data are assigned to corresponding skeletons, the hand skeleton is driven to move through an IK algorithm, the pedals are changed in angle and slide up and down by stepping on the pedal group, the speed and the angle of the airplane are controlled, screen display and flight data display are performed, better real data can be obtained, and an external operator can conveniently sort the data, so that a better experience value is obtained.
2. The flight special situation handling experience system and the operation method thereof process through a plurality of different tests, including fire special situations: simulating the fire accident of the airplane and simulating the fire extinguishing process; special condition of lubricating oil: simulating the oil lubrication fault of the airplane and simulating the oil lubrication treatment process; special case of flight interruption: accidents occur in the aircraft takeoff process, or takeoff action operation flow simulation is temporarily cancelled, and the reaction capability and the various strain capabilities of the aircraft drivers can be tested through various simulation operation treatments, so that the aircraft drivers can conveniently operate and treat the aircraft.
Drawings
FIG. 1 is a block diagram of the working principle of the present invention;
FIG. 2 is a schematic view of the internal structure of the pedal set according to the present invention;
FIG. 3 is a schematic view of the internal structure of a data glove of the present invention;
FIG. 4 is a schematic diagram of the internal structure of the head display device according to the present invention;
fig. 5 is a schematic diagram of the internal structure of the base station according to the present invention.
In the figure: 1. a pedal group; 2. a direction axis; 3. a brake shaft; 4. an RJ12 male connector; 5. a USB adapter; 6. an RJ12 female connector; 7. a USB connector; 8. a selector switch; 9. an LED display; 10. a heel cushion; 11. an inner hexagonal wrench; 12. a data glove; 13. a capture locator; 14. a sensor; 15. a head display device; 16. an operating handle; 17. an output device; 18. a base station; 19. a status indicator light; 20. a channel indicator light; 21. a front panel; 22. a power port; 23. a channel button; 24. a data line port; 25. a USB port; 26. a PC host; 27. a sensing locator.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-2, the present invention provides a technical solution: a flight special situation disposal experience system comprises a pedal group 1, a data glove 12, a head display device 15, a base station 18 and a PC host 26, wherein the output ends of the data glove 12 and the pedal group 1 are electrically connected with the input end of the PC host 26, the internal data of the data glove 12 and the pedal group 1 can be transmitted into the PC host 26, the PC host 26 is in bidirectional connection with the head display device 15, the internal data of the head display device 15 can be transmitted into the PC host 26 in real time, the PC host 26 can process the data in real time, the head display device 15 is in bidirectional connection with a capture locator 13 and a perception locator 27 respectively, the capture locator 13 and the perception locator 27 are laser locators, the capture locator 13 and the perception locator 27 can transmit positioning data into the head display device 15 in real time, and drivers and passengers can feel driving better;
an inner hexagonal wrench 11 is placed at one side position of a pedal group 1, brake shafts 3 are fixedly installed at two sides of the upper end face of the pedal group 1, a direction shaft 2 is fixedly installed at the middle position of the upper end face of the pedal group 1, a heel back cushion 10 is fixedly installed at the position, close to the lower end position, of the inclined plane of each brake shaft 3, the pedals are enabled to change the angle and slide up and down by stepping on the pedal group 1, the speed and the angle of an airplane are controlled, an RJ12 male connector 4 is electrically connected at one side position of the pedal group 1, a USB adapter 5 is electrically connected at one side of the RJ12 male connector 4, an LED display 9 is fixedly installed at the upper end face of the USB adapter 5, the LED display 9 can display the working state inside the USB adapter 5 in real time, an RJ12 female connector 6 is fixedly installed at the outer surface of one side of the USB adapter 5, a selector switch 8 is fixedly installed at the position, close to the middle position of the lower end face of the front end face of the USB adapter 5, the position of one end of the USB adapter 5 is electrically connected with a USB connector 7, the position of the RJ12 male connector 4 corresponds to the position of the RJ12 female connector 6, the pedal group 1 can be better connected with the USB adapter 5 through the RJ12 male connector 4 and the RJ12 female connector 6, the inner hexagonal wrench 11 is of a hexagonal structure, and the inner hexagonal wrench 11 is convenient for external personnel to maintain;
referring to fig. 3-5, a capturing positioner 13 is fixedly installed at the back of the hand on the outer surface of the data glove 12, a plurality of sensors 14 are fixedly installed at the finger positions on the outer surface of the data glove 12, the data glove 12 acquires hand skeleton information through the sensors 14 and transmits the hand skeleton information to an application program, the application program further calculates skeleton data, then assigns the data to corresponding skeletons, and drives the hand skeleton to move through an IK algorithm, a head display device 15 includes an operation handle 16 and an output device 17, the operation handle 16 and the output device 17 are both wirelessly connected with the head display device 15, a specific gesture is triggered according to different actions of the hand, the operation handle 16 and the virtual key are triggered, so as to achieve the effect of really operating the airplane, a front panel 21 is fixedly installed at the middle position of the front end surface of the base station 18, a status indicator lamp 19 is fixedly installed at the middle position of the upper end of the front panel 21 at the front end surface of the base station 18, a channel indicator lamp 20 is fixedly arranged at the position of one side corner of a front panel 21 on the front end face of a base station 18, a channel button 23 is fixedly arranged at the position of one side corner of the rear end face of the base station 18 close to the middle of the lower end, a data cable port 24 is fixedly arranged at the position of the other side of the rear end face of the base station 18 close to the middle of the lower end, a power port 22 is fixedly arranged at the position of one side corner of the rear end face of the base station 18, a USB port 25 is fixedly arranged at the position of the other side corner of the rear end face of the base station 18, the flight special situation can be simulated and treated by combining the change of the flight state with the sound and the special effect, the state indicator lamp 19 and the channel indicator lamp 20 are electrically connected with an external power supply and an external switch, external connecting wires are arranged inside the data cable port 24, the power port 22 and the USB port 25, the base station 18 can work through the connecting action of the external connecting wires, and the annular surface of an operating handle 16 is wrapped by rubber pads, the anti-skidding line has been seted up to rubber pad annular surface, when avoiding outside personnel to hold between the fingers, takes place to skid.
Further, the operation method of the flight special situation handling experience system comprises the following steps:
step one, building an airplane three-dimensional model according to a proportion, and building a runway and an airport scene;
mounting each component in the engine on an airplane model to enable the airplane to have a real physical effect;
thirdly, the data glove 12 acquires hand skeleton information through the sensor 14 and transmits the hand skeleton information to an application program, the application program further calculates skeleton data, then assigns the data to corresponding skeletons, and drives the hand skeleton to move through an IK algorithm;
triggering specific gestures according to different actions of the hands to complete the control of the operating handle 16 and the triggering of the virtual keys, so as to achieve the effect of really controlling the airplane;
step five, the pedal group 1 is stepped by feet to enable the pedals to change the angle and slide up and down, and the speed and the angle of the airplane are controlled;
step six, finishing a series of operations such as taking off, flying, landing and the like of the airplane by combining the step 4 and the step 5;
and seventhly, simulating and disposing the special flight situation by combining the sound and the special effect and changing the flight state.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides a flight special case deals with experience system, includes pedal group (1), data gloves (12), head shows equipment (15), base station (18) and PC host computer (26), its characterized in that: the output ends of the data glove (12) and the pedal group (1) are electrically connected with the input end of a PC host (26), the PC host (26) is bidirectionally connected with a head display device (15), the head display device (15) is respectively bidirectionally connected with the capturing positioner (13) and the perception positioner (27), and the capturing positioner (13) and the perception positioner (27) are both laser positioners;
an inner hexagonal wrench (11) is arranged at one side of the pedal group (1), brake shafts (3) are fixedly arranged on two sides of the upper end surface of the pedal group (1), a direction shaft (2) is fixedly arranged at the middle position of the upper end surface of the pedal group (1), a heel back cushion (10) is fixedly arranged at the position of the inclined plane of the brake shaft (3) close to the lower end, one side of the pedal group (1) is electrically connected with an RJ12 male connector (4), one side of the RJ12 male connector (4) is electrically connected with a USB adapter (5), an LED display (9) is fixedly arranged on the upper end surface of the USB adapter (5), the outer surface of one side of the USB adapter (5) is fixedly provided with an RJ12 female connector (6), a selector switch (8) is fixedly arranged at the middle position of the front end surface of the USB adapter (5) close to the lower end, one end of the USB adapter (5) is electrically connected with a USB joint (7).
2. The system of claim 1, wherein: the outer surface of the data glove (12) is fixedly provided with a plurality of sensors (14) at finger positions, and data lines are fixedly connected among the sensors (14).
3. The system of claim 1, wherein: the head display equipment (15) comprises an operating handle (16) and output equipment (17), and the operating handle (16) and the output equipment (17) are both in wireless connection with the head display equipment (15).
4. The system of claim 1, wherein: the utility model discloses a communication terminal, including base station (18), terminal surface intermediate position department fixed mounting has front panel (21) before base station (18), the terminal surface is located front panel (21) upper end intermediate position department fixed mounting has status indicator lamp (19) before base station (18), the terminal surface is located front panel (21) one side angular position department fixed mounting has channel pilot lamp (20) before base station (18), base station (18) rear end face is close to one side position department fixed mounting in the middle of the lower extreme has channel button (23), base station (18) rear end face is close to the other side position department fixed mounting in the middle of the lower extreme has data line port (24), base station (18) rear end face one side angular position department fixed mounting has power port (22), base station (18) rear end face opposite side angular position department fixed mounting has USB port (25).
5. The system of claim 4, wherein: the status indicator lamp (19) and the channel indicator lamp (20) are electrically connected with an external power supply and an external switch, and external connecting wires are arranged inside the data line port (24), the power supply port (22) and the USB port (25).
6. The system of claim 3, wherein: the annular outer surface of the operating handle (16) is wrapped with a rubber pad, and the annular outer surface of the rubber pad is provided with anti-skid grains.
7. The system of claim 1, wherein: the position between RJ12 male joint (4) and RJ12 female joint (6) corresponds, interior hexagonal spanner (11) are the hexagon structure.
8. A flight specific situation handling experience system according to any one of claims 1 to 7, the method of operation comprising the steps of:
step one, building an airplane three-dimensional model according to a proportion, and building a runway and an airport scene;
mounting each component in the engine on an airplane model to enable the airplane to have a real physical effect;
thirdly, the data glove (12) acquires hand skeleton information through the sensor (14) and transmits the hand skeleton information to the application program, the application program further calculates skeleton data, then assigns the data to corresponding skeletons, and drives the hand skeleton to move through a worker K algorithm;
triggering specific gestures according to different actions of the hand, completing the control of the operating handle (16) and the triggering of the virtual keys, and achieving the effect of really controlling the airplane;
step five, the pedal group (1) is stepped by feet to enable the pedals to change the angle and slide up and down, and the speed and the angle of the airplane are controlled;
step six, finishing a series of operations such as taking off, flying, landing and the like of the airplane by combining the step 4 and the step 5;
and seventhly, simulating and disposing the special flight situation by combining the sound and the special effect and changing the flight state.
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CN202010683430.3A CN113947969A (en) | 2020-07-15 | 2020-07-15 | Flight special situation disposal experience system and operation method |
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CN202010683430.3A CN113947969A (en) | 2020-07-15 | 2020-07-15 | Flight special situation disposal experience system and operation method |
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CN110738901A (en) * | 2019-11-28 | 2020-01-31 | 西安飞豹科技有限公司 | flight simulator |
CN213634943U (en) * | 2020-07-15 | 2021-07-06 | 北京易智时代数字科技有限公司 | Experience system is dealt with to special feelings of flight |
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2020
- 2020-07-15 CN CN202010683430.3A patent/CN113947969A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN107221223A (en) * | 2017-06-01 | 2017-09-29 | 北京航空航天大学 | A kind of band is strong/the virtual reality aircraft cockpit system of touch feedback |
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Application publication date: 20220118 |