CN110520918A - Spacecraft flight simulator - Google Patents
Spacecraft flight simulator Download PDFInfo
- Publication number
- CN110520918A CN110520918A CN201780089592.0A CN201780089592A CN110520918A CN 110520918 A CN110520918 A CN 110520918A CN 201780089592 A CN201780089592 A CN 201780089592A CN 110520918 A CN110520918 A CN 110520918A
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- China
- Prior art keywords
- spacecraft
- simulator
- seat
- control
- flight
- 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.)
- Pending
Links
- 238000010276 construction Methods 0.000 claims abstract description 9
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 6
- 230000001133 acceleration Effects 0.000 claims description 5
- 230000010355 oscillation Effects 0.000 claims description 3
- 238000013519 translation Methods 0.000 claims description 3
- 238000012800 visualization Methods 0.000 claims description 3
- 230000006698 induction Effects 0.000 abstract 4
- 230000003287 optical effect Effects 0.000 abstract 1
- 238000003032 molecular docking Methods 0.000 description 12
- 238000013461 design Methods 0.000 description 5
- 238000000926 separation method Methods 0.000 description 4
- 238000012549 training Methods 0.000 description 4
- 238000003384 imaging method Methods 0.000 description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000004088 simulation Methods 0.000 description 3
- 230000003068 static effect Effects 0.000 description 3
- 239000002775 capsule Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000002828 fuel tank Substances 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000012634 optical imaging Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- 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
- G09B9/52—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of an outer space vehicle
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)
- Toys (AREA)
Abstract
The present invention relates to the simulator for manned spacecraft, the simulator is equipped with electronic display system and optical observation system, and can be used for amusement or aims of education, and the purpose is to develop the technical ability of control Soyuz spacecraft.Spacecraft flight simulator includes the support construction with induction element, and is designed to the pitching frame for the hemisphere format that can be shifted along induction element.Vertical support structure is arranged at the front of user's seat, is connected to pitching frame and the tables including having the induction element for translational movement.Induction element have control handle and be arranged at vertical support top and including the control of side monitor backstage.The solution have the advantages that extending the Functional Capability of space mission simulator.
Description
Technical field
The present invention relates to the simulators equipped with number and the manned spacecraft of optical imaging system.The simulator can be by
For amusement and aims of education, the purpose is to instruct the driving efficiency in relation to Soyuz (Soyuz) spacecraft, to educate without weight
The movement physics of solid under power.
Background technique
A kind of prior art: flight simulator seat (Russian Federation patent imitated with vibration/shock
No.2555053,07/10/2015), seat base, the vibration/shock Mechanical Driven dress of damping supporting seat are attached to including its pillar
Set and using standard seal sound system, wherein vibration/shock mechanical actuation device is by the business that is located in chest
Available subwoofer (subwoofer) is constituted, and output port is covered with the rubber for being attached to one end of a connecting rod
Diaphragm, the other end of connecting rod are attached to Standard Flight person's seat.
The equipment (is gone straight up to by visual imaging and truly feels (sound, promotion and impact) to imitate actual spacecraft
Machine etc.) cabin ambient.This user's offer immersion that is designed as in-flight is experienced.
One of the design the disadvantage is that due to seat be it is static, function is restricted, it means that Yong Huwu
The flight and analog case that seat will be tilted or be deviated during method is experienced completely.
Another prior art is that (Russian Federation patent No.130733, date be for a kind of aircraft simulator
07/27/2013), including with pilot seat cockpit, flight control assemblies, video imaging system, pitching rotating frame,
Have crutched pedestal and pitching/axial-rotation driving device, wherein cockpit be installed in inside pitching rotating frame and
It can be rotated around its fore and aft axis, which is installed between pedestal column by two carrying supports, pitching rotating frame
York piece including being attached to cockpit, with damper (silent block) carry placing device and around cockpit perpendicular to
The annulus of york piece plane；There are at least three idler wheels in present portion out of my cabin, and the idler wheel is installed into can roll on annulus；And
Pedestal column, which carries placing device, has damper.Additional equipment can be used for the experience of more immersion: stereo, lamp
Light, air-flow, vibration, cooling, heating etc..Flight simulator for pilot training allows controlled and unrestricted
Cockpit is mobile: inclination (left and right), pitching (upper and lower) and the bidirectional rotation around its axis.Various movements can be individually or
Combination, it is motor-driven to simulate aerobatics.Video imaging system shows three-dimensional (3D) image to user, and there are also to produce
The equipment of raw special efficacy.
But pitch drive is complicated and heavy, and occupies many additional spaces.In addition, control device (control
Panel processed) and seat be located in the cockpit that is limited to, and the height, size and other features of user can not be adjusted to match
(such as user is children or adult), to limit simulator function.
Russian Federation patent No.2367027 (date 09/10/2009) discloses a kind of manned spacecraft (Don-
Soyuz-TMA, Soyuz-TMA) simulator, the prior art which is closest to.The simulator includes return capsule material object
Model (mock-up), the mock-up have TV monitoring and controlling video camera, ground control to spacecraft radio link simulations device,
Control stick, periscope window, gesture stability control stick, sound system, window, flight engineer's seat, commanding officer's seat, aerospace
Member's research institute's seat and flight control and visualization software.
The return capsule mock-up is the static shell with static crew's seat.It can not true simulation space flight
Flight experience, to also indicate that the function of proposed design is restricted.
Summary of the invention
The solution have the advantages that the real-life being adjusted by compact design with the specific features for user
Space travel experience combination and extend spacecraft flight simulator function.
Described have the technical effect that realizes that by a kind of spacecraft flight Simulator design, the design includes: support knot
Structure is attached to the guide device of support construction, and the semicircle pitching frame that can be slided along guide device is attached to pitching frame
The seat of frame, the plumb post being mounted in front of seat, which is attached to pitching frame and carries, and there is translation to move
The tables of dynamic guide device, control stick is disposed thereon, the control panel with side monitor at the top of plumb post, pitching frame
Frame driving device, for vertical (along the plumb post) driving device of the control panel with side monitor, flight control
With visualization hardware and software, sound system, and the oscillation drive of imitation acceleration.
All components listed of simulator claimed are all located in its support construction, thus keep its compact and
It is convenient to use to locate in any position.Flight control and visualization software, pitching frame guide device and sound system offer connect
Nearly true space travel experience.The driving device that vertically moves of control panel with side monitor makes training/game
It can be used for any user, either children or adult.In view of advantage mentioned above, the new product will successfully with it is similar
Equipment be at war with.
Detailed description of the invention
Fig. 1 shows the general arrangement of spacecraft flight simulator.
Fig. 2 shows side view of the spacecraft flight simulator in its initial configuration.
Fig. 3 shows side view of the spacecraft flight simulator in its operative configuration.
Fig. 4 shows the top view of spacecraft flight simulator.
Specific embodiment
Spacecraft flight simulator includes: support construction 1, is attached to the guide device 2 of support construction 1, can be along drawing
The semicircle pitching frame 3 for leading the sliding of device 2, is attached to the seat 4 of pitching frame 3, is mounted on the plumb post in 4 front of seat
5, which, which is attached to pitching frame 3 and carries, has the tables 6 for being moved in translation guide device 7, and control stick 8 is located at
Wherein, the control panel 9 with side monitor 10 at 5 top of plumb post, pitching frame driving device (not shown) have
The control panel of side monitor vertically moves driving device (along plumb post；It is not shown), flight control and visualization
Hardware and software (not shown), sound system (not shown), and imitate acceleration oscillation drive (not shown) (Fig. 1,
2、3)。
1 annulus made of seamless pipe of support construction is constituted.Corrugation platform and ladder are installed in the structure.
Pitching frame 3 is the semicircular ring made of seamless pipe.
Guide device 2 is bending track guide device, and pitching frame 3 is advanced along it.
Pitching frame driving device is that pitching frame is driven from the cable electric power that its initial position is moved to its operating position
Dynamic device.The driving device is made of crane (hoist), cable and pulley with preloader.These components be located at watt
The bottom of support construction 1 below stupefied platform.
It can also carry out movable pitching frame, using actuator to replace previously described electric crane and cable to drive dress
It sets.
Control panel with side monitor vertically moves driving device (along plumb post 5) by being located at control plane
9 inside of plate and power-driven gear (actuator) composition for being in its central part for being attached to plumb post 5.
Tables 6 are the metal surfaces with the translational movement guide device 7 adhered to therewith.
Control stick 8 is made of Spacecraft Attitude Control device (SAC) and manual Spacecraft Control device (MSC).In addition there are drops
Fall controller (DC).
Acceleration imitates driving device and is installed in under-seat and is in the rear of seat back.It imitates different fly
The vibration and impact of row order section: close, docking, is returned and is landed separation.
Sound system is made of the loudspeaker with mini subwoofer (mini subwoofer).It is generated
Sound in the true launch and flight of Soyuz spacecraft.Sound system is located at the lower section of metal tables 6.Cable can be by cloth
Line can be embedded in control panel 9 in the inside of control panel 9, loudspeaker.
Soyuz spacecraft flight simulator is intended for amusement and aims of education.It can be used in Technology Park, theme
Park and children education center, Science Museum and other museums, educational institution, shopping center and other recreational facilities
In.
All simulator options all include basic software, are allowed from 100 meters of distance close to international space station
(ISS)；The different craft ports being docked in space station；Adjustable time and lighting condition；Three from new hand to astronaut
A training/grade of skill；And docking performance appraisal.
The minimum use age is 8 years old.
Each number of users is 1.
It can be answered by simulator operator by selection the users ' skills grade and introducing emergency to configure flight plan
Miscellaneous degree.
Software has the pause feature that can be activated at any time.Then restore to fly with preset condition.
Side monitor shows the Soyuz spacecraft on the transmitting station of the spaceport Baikonur (space launching site), band
There are the rocket launching of Soyuz spacecraft and the overview view of rocket and spacecraft flight, stage separation and Earth's orbit entrance
Frequently；And for ISS close to the periscope video with docking operation.Side monitor is also shown about Soyuz spacecraft state
Information；Information about offline mode；ISS dynamic image under different orientations；About the success for holding winged Soyuz spacecraft
With the result of unsuccessful user action；And user's performance appraisal.
Simulator may include showing (multiple) external screen of simulator demonstration video or image being replicated in side
On the monitor of face.
Here is the overview operated for the spacecraft flight simulator of different offline mode.
As demonstration starts, side monitor shows Soyuz spacecraft from 800 meters of distance close to ISS.Control panel
Show spacecraft status data；The moving map of the earth shows the current Space Vehicle position in the track relative to the earth.
Before flight during bulletin, user is entered in seat, tenses safety belt, and receive and instruct from instruction person.This
One stage can continue the time of necessary length, until instruction person presses " ignition key " (" beginning ") button.
Side monitor shows following information:
Left monitor shows the omni-directional camera view of Baikonur transmitting station.15-30 seconds when the duration
(view of transmitting station and rocket)；
Right monitor shows transmitting station (top view) (or the left window view) from airborne photogrammetric camera.
Control panel shows spacecraft status service information and has Soyuz spacecraft and the current location ISS and rail
The Earth map of mark.
The seat that the rising of spacecraft starts from user is moved to flight position to match astronaut in true Soyuz
Position in spacecraft.Seat position is kept, until crew enters ISS.Subsequent instruction person presses start button.
Once seat is in flight position, side monitor then shows the video that rocket goes up to the air from transmitting station.Control plane
Plate monitor shows current spacecraft status data.
After the transmission, side window shows the acceleration video (transmitting with the transmitting sequence of spacecraft injection
The separation of escape system [LES] tower, rectification housing fall off, and engine opens and closes, stage separation, spacecraft injection, the sun
Energy panel deployment etc.).
During Soyuz transmitting is entered the orbit, side monitor alternately shows the earth, the sun and starry sky.
ISS is subsequently activated close to mode, and side monitor shows Soyuz close to ISS.Control panel is aobvious
Current data about spacecraft state is shown.
When instruction person activates automatic docking mode, user does not need to do anything, it is only necessary to enjoy flight and docking
Simulation.
For approaching and docking manually, at a distance from ISS apart about 100 meters, emergency (ES) occurs: automatic
Change docking failure (having alarm), therefore user must approach manually and be docked to ISS.
The close and docking period is limited by the quantity of fuel in time and fuel tank.It is possible the result is that: successfully
Soyuz to ISS docking；Spacecraft is flown in space；And the collision between spacecraft and space station.
SAC and MSC control stick is used to control spacecraft maneuver.
In the case where failure is attempted in docking, spacecraft can be returned to start bit by software (under the decision of operator)
It sets, and another docking is implemented with identical or different complexity level and is attempted.Each complexity level has its own
Starting distance (30,50,100 meters), the fuel limitation in the time restriction for docking and fuel tank.
After the game is over, side monitor show the control about Soyuz spacecraft user's performance results and
Assessment.
After training/game over, instruction person presses stop button, resets pitching frame, and unlock safety belt.With
Family then may exit off seat.
Simulator claimed can be pre-adjusted to match specific user characteristics (height, body parameter
Etc.).Control panel with side monitor can be set at so that user sees screen and controls in which can be convenient
The height of simulated flight.All components are all located in circular support structure, so that simulator is compact.
Claims (1)
1. a kind of spacecraft flight simulator, characterized by comprising: support construction is attached to the guide device of support construction,
The semicircle pitching frame that can be slided along guide device, is attached to user's seat of pitching frame, is mounted in front of seat
Plumb post, the plumb post be attached to pitching frame and carry have be moved in translation guide device tables, control stick
It is disposed thereon, the control panel with side monitor at the top of plumb post, pitching frame driving device, for having
Vertical (along the plumb post) driving device of the control panel of side monitor, flight control and visualization hardware and software,
Sound system, and imitate the oscillation drive of acceleration.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2017117643 | 2017-05-22 | ||
| RU2017117643A RU2653448C1 (en) | 2017-05-22 | 2017-05-22 | Simulator of space flight of a space vehicle |
| PCT/RU2017/000389 WO2018217121A1 (en) | 2017-05-22 | 2017-06-07 | Spacecraft flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110520918A true CN110520918A (en) | 2019-11-29 |
Family
ID=62105704
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780089592.0A Pending CN110520918A (en) | 2017-05-22 | 2017-06-07 | Spacecraft flight simulator |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN110520918A (en) |
| RU (1) | RU2653448C1 (en) |
| WO (1) | WO2018217121A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2761587C1 (en) * | 2021-04-15 | 2021-12-10 | федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королева" | Interactive educational and methodological complex simulating the target operating of the earth remote sensing spacecraft |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1304810C (en) * | 1987-10-22 | 1992-07-07 | Greg W. Berg | Video simulation apparatus |
| US20070054592A1 (en) * | 2005-09-02 | 2007-03-08 | Chang Young J | Seat-driving device for simulation system |
| RU2367027C1 (en) * | 2008-02-05 | 2009-09-10 | Общество с ограниченной ответственностью "Центр тренажеростроения и подготовки персонала" | Manned spacecraft simulator |
| CN101842822A (en) * | 2007-12-24 | 2010-09-22 | 罗伯特·奇尔德雷斯 | Motion platform video game racing and flight simulator |
| CN202632581U (en) * | 2012-05-28 | 2012-12-26 | 戴震宇 | Flight simulation control and experience device based on real air environment |
| CN204143671U (en) * | 2014-09-15 | 2015-02-04 | 孙波 | Race simulator |
| CN206039947U (en) * | 2016-05-20 | 2017-03-22 | 钟君城 | Initiative control platform about VR |
| CN206115768U (en) * | 2016-07-07 | 2017-04-19 | 上海源荀电子技术有限公司 | Modularization simulation passenger cabin device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2425667C1 (en) * | 2010-03-01 | 2011-08-10 | Леонид Андреевич Косик | Device for creation of space disorientation in people |
-
2017
- 2017-05-22 RU RU2017117643A patent/RU2653448C1/en active IP Right Revival
- 2017-06-07 WO PCT/RU2017/000389 patent/WO2018217121A1/en active Application Filing
- 2017-06-07 CN CN201780089592.0A patent/CN110520918A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1304810C (en) * | 1987-10-22 | 1992-07-07 | Greg W. Berg | Video simulation apparatus |
| US20070054592A1 (en) * | 2005-09-02 | 2007-03-08 | Chang Young J | Seat-driving device for simulation system |
| CN101842822A (en) * | 2007-12-24 | 2010-09-22 | 罗伯特·奇尔德雷斯 | Motion platform video game racing and flight simulator |
| RU2367027C1 (en) * | 2008-02-05 | 2009-09-10 | Общество с ограниченной ответственностью "Центр тренажеростроения и подготовки персонала" | Manned spacecraft simulator |
| CN202632581U (en) * | 2012-05-28 | 2012-12-26 | 戴震宇 | Flight simulation control and experience device based on real air environment |
| CN204143671U (en) * | 2014-09-15 | 2015-02-04 | 孙波 | Race simulator |
| CN206039947U (en) * | 2016-05-20 | 2017-03-22 | 钟君城 | Initiative control platform about VR |
| CN206115768U (en) * | 2016-07-07 | 2017-04-19 | 上海源荀电子技术有限公司 | Modularization simulation passenger cabin device |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018217121A1 (en) | 2018-11-29 |
| RU2653448C1 (en) | 2018-05-08 |
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| PB01 | Publication | ||
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Application publication date: 20191129 |