CN205645015U - Ground passenger cabin and two -degree -of -freedom 360 degree flight driving simulation cabin emulation motion platform - Google Patents
Ground passenger cabin and two -degree -of -freedom 360 degree flight driving simulation cabin emulation motion platform Download PDFInfo
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- CN205645015U CN205645015U CN201620008466.0U CN201620008466U CN205645015U CN 205645015 U CN205645015 U CN 205645015U CN 201620008466 U CN201620008466 U CN 201620008466U CN 205645015 U CN205645015 U CN 205645015U
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Abstract
The utility model provides a ground passenger cabin and two -degree -of -freedom 360 degree flight driving simulation cabin emulation motion platform, include passenger cabin body, luffing drive module and control rotary motion drive module, the luffing drive module drive the passenger cabin body carries out luffing, control the rotary motion drive module drive rotary motion about the passenger cabin body. Luffing drive module includes fixing machine pallet, first motor, it includes passenger cabin motion support frame, second motor and passenger cabin support to control rotary motion drive module. The utility model discloses well ground passenger cabin simple structure, it is rationally distributed, can realize 360 degrees rotations.
Description
Technical field
This utility model relates to flight simulation test, in particular it relates to a kind of ground passenger cabin and 360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom.
Background technology
As the General Aviation industry of one of 21 century rising industry, the important function in the national economic development highlights day by day, and the development environment of General Aviation industry is increasingly mature, has great demand at aspects such as agricultural flight, forest extinguishing, aviation emergency management and rescue.Have great importance simultaneously for prosperous and powerful civil aviation industry.
Civil aviaton of the U.S. has aircraft 230,000 multi rack now, and wherein general aviation aircraft accounts for about 96%；Having pilot more than 70 ten thousand, wherein General Aviation Flight person accounts for the overwhelming majority；Organic field more than 1.75 ten thousand, wherein navigation airport accounts for about 96%.And the situation of China allows of no optimist under comparing, by the end of the year 2010, General Aviation airport, interim landing point have 329, wherein hold civil airport and use the General Aviation airport of licence, 44, landing field, General Aviation opportunity airfield (landing point) 285.Overall Airport Resources is weaker, can not meet the fast-developing needs of General Aviation.Meanwhile, in terms of the resource of spatial domain, China spatial domain resource management and exploitation do not catch up with, spatial domain and air route resource scarcity.The reasons such as the air traffic control technology of China is the most backward, and ATC Facilities is under-capitalized, and airspace management system is the most perfect, use spatial domain program is unfamiliar with by the common people, limit the fast development of General Aviation.
China's navigation industry has huge development potentiality, future will be added to about 10000 framves for 5 to 10 years, and annual rate of growth reaches 30%, pulls the experience of industrial chain development 1:10 according to aviation, following 10 years General Aviations pull on 1,000,000,000,000 demands, will become China's socio-economic development new growth point.Referring again to before 10 years and the car steering training industry of today, we are just it is conceivable that the future development of navigation.But the development of this industry but to receive time, fund cost big, spatial domain is examined, the restriction of the aspect factors such as weather and human resources's shortage, such as fly true aircraft price about in 9000 RMB per hour, the acquisition of business's photograph needs the training expense of about 700,000, two cards of spatial domain examination & approval to have extremely complex flow process etc..
If a kind of approach solving these problems is exactly the driving cabin in aircraft to be moved on ground, pilot manipulating in the face of aerial aircraft on ground, the driving cabin on ground has again the sensation of airflight simultaneously, such as what comes into a driver's and body-sensing.
Thus general thinking is such that a driving cabin that can operate aerospace plane or unmanned plane on the ground；Transmitted true what comes into a driver's by aerial aircraft or unmanned plane and return to driving cabin, it is thus achieved that aerial true what comes into a driver's；Sensor records flight parameter and transmits to moving platform, makes ground driving cabin obtain body-sensing.Allow driver obtain the true what comes into a driver's of airflight in the driving cabin of ground, reduce the true body-sensing driven an airplane as far as possible.Ground flying simultaneously in turn ensure that safety, economy.
This by ground driving cabin manipulation aerospace plane is remembered with gratitude, proposes the earliest at the beginning of 1980.It is the control rate testing Rafale aircraft with A319 at that time.The method of this test, is by carrying out, at the driving cabin on ground, the A319 that remote control is aerial, tests and will be used for the control rate on Rafale aircraft.
Utility model content
For defect of the prior art, the purpose of this utility model is to provide a kind of ground passenger cabin and 360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom.
The ground passenger cabin provided according to one aspect of this utility model, drives module and left-right rotation to drive module including Cab body, elevating movement；Described elevating movement drives Cab body described in module drive to carry out elevating movement, and described left-right rotation drives Cab body left-right rotation described in module drive.
Preferably, described elevating movement drives module to include fixed frame platform, the first motor；Described left-right rotation drives module to include passenger cabin kinematic mount frame, the second motor and passenger cabin support；
Described first motor is arranged on described fixed frame platform；On described passenger cabin kinematic mount frame and described fixed frame table-hinges；Described first motor drives described passenger cabin kinematic mount frame to carry out pitch rotation；
The upper end of described passenger cabin support is hinged with the upper end medial surface of described passenger cabin kinematic mount frame, and lower end is hinged with the lower end inside face of described passenger cabin kinematic mount frame, thus described passenger cabin support can circumferentially rotate；
Described second motor is arranged on passenger cabin kinematic mount frame, and described second motor drives described passenger cabin support to be rotated；Described Cab body is arranged in described passenger cabin support.
Preferably, described fixed frame platform includes base supporting part and the longitudinal bracing portion being vertically connected；
Described passenger cabin kinematic mount frame is arranged in described longitudinal bracing portion and is located at the upside of described base supporting part；
Described passenger cabin support is cage type.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that another aspect of this utility model provides, described ground passenger cabin, also includes unmanned plane, ground passenger cabin, the first communication module, the second communication module, the first control module and the second control module；
Wherein, described unmanned plane is provided with Position and attitude sensor, the first communication module and the first control module；Described Position and attitude sensor is for measuring the angle of pitch and the left and right swing angle of unmanned plane；Described first control module connects Position and attitude sensor and the first communication module；
Described second control module connects described elevating movement and drives module, described left-right rotation to drive module and the second communication module；
Described first control module is obtained the described angle of pitch and left and right swing angle and is sent by described first communication module；Described second control module receives the described angle of pitch and described left and right swing angle by described second communication module, and then control described elevating movement driving module rotation according to the described angle of pitch, control described left-right rotation according to described left and right swing angle and drive module to rotate.
Described passenger cabin kinematic mount frame is arranged in described longitudinal bracing portion and is located at the upside of described base supporting part.
Preferably, described first control module and/or described second control module use arduino single-chip microcomputer.
Preferably, display is also included；
Wherein, in described display is arranged on described ground passenger cabin；Described display electrically connects described second control module.
Preferably, during described Position and attitude sensor includes such as lower sensor any one or appoint multiple:
-acceleration transducer；
-Position and attitude sensor；
-torque sensor.
Preferably, body monitoring device and alarm device are also included；
Wherein, described body monitoring device electrically connects described second control module；Described body monitoring device is for the condition detecting simulated flight personnel and the accekeration being subject to, and described condition and the acceleration being subject to is sent to described second control module to set time threshold；
Described alarm device electrically connects described second control module, and when described condition is less than setting threshold value, or the acceleration being subject to is more than when setting threshold value, and described alarm device sends alarm signal；
Described condition includes in heart rate, respiratory frequency and body temperature any one or appoints multiple.
Preferably, photographic head is also included；
Multiple described photographic head are arranged on front end face and the two sides of described unmanned plane；Multiple described photographic head connect described first control module；
The image information of described camera collection is sent by described first control module by described first communication module；Described second control module receives described image information by described second communication module, and then sends described image information to the broadcasting of described display.
Compared with prior art, this utility model has a following beneficial effect:
1, this utility model relies on unmanned plane safety high, and the outstanding advantage of low cost utilizes the true what comes into a driver's of unmanned plane, can obtain on ground and the most close flight experience, the enjoyment of Feel Flight in Action；Relying on this system, pilot can perform the test mission of navigation flivver on ground, and the test mission of complete the to take off series of complexes such as landing, stall test, test flight envelope curve, flight test people's safety is greatly ensured；
2, this utility model can be real-time transmission what comes into a driver's and flying quality, carry out image mosaic in cabin is driven on ground, data parsing processes, pilot can obtain and the what comes into a driver's of aerial practical operation on the ground, extensive application can be developed by the flight with true what comes into a driver's, fill up the application of navigation aircraft or perform hot mission；
3, in this utility model, ground cockpit structure is simple, rationally distributed, it is possible to realize 360 degree of rotations.
Accompanying drawing explanation
The detailed description with reference to the following drawings, non-limiting example made by reading, other features, objects and advantages of the present utility model will become more apparent upon:
Fig. 1 is the structural representation of 360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom in this utility model；
Fig. 2 is the structural representation of ground passenger cabin in this utility model.
In figure:
1 is the second motor；
2 is the first motor；
3 is passenger cabin support；
4 is fixed frame platform；
5 is passenger cabin kinematic mount frame.
Detailed description of the invention
Below in conjunction with specific embodiment, this utility model is described in detail.Following example will assist in those skilled in the art and are further appreciated by this utility model, but limit this utility model the most in any form.It should be pointed out that, to those skilled in the art, without departing from the concept of the premise utility, it is also possible to make some deformation and improvement.These broadly fall into protection domain of the present utility model.
In the present embodiment, 360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, including unmanned plane, ground passenger cabin, the first communication module, the second communication module, the first control module and the second control module；
Wherein, described unmanned plane is provided with Position and attitude sensor, the first communication module and the first control module；Described Position and attitude sensor is for measuring the angle of pitch and the left and right swing angle of unmanned plane；Described first control module connects Position and attitude sensor and the first communication module；
Described ground passenger cabin includes that Cab body, elevating movement drive module and left-right rotation to drive module；Described elevating movement drives module to be used for driving described Cab body to carry out elevating movement, and described left-right rotation drives module to be used for driving described Cab body left-right rotation；
Described second control module connects described elevating movement and drives module, described left-right rotation to drive module and the second communication module；
Described first control module is obtained the angle of pitch and left and right swing angle and is sent by described first communication module；Described second control module receives the described angle of pitch and described left and right swing angle by described second communication module, and then control described elevating movement driving module rotation according to the described angle of pitch, control described left-right rotation according to described left and right swing angle and drive module to rotate.
Described elevating movement drives module to include fixed frame platform the 4, first motor 2；Described left-right rotation drives module to include passenger cabin kinematic mount frame the 5, second motor 1 and passenger cabin support 3；
Described first motor 2 is arranged on described fixed frame platform 4；Described passenger cabin kinematic mount frame 5 and described fixed frame platform 4 cut with scissors；Described first motor 2 drives described passenger cabin kinematic mount frame 5 to carry out pitch rotation；
The upper end of described passenger cabin support 3 is hinged with the upper end medial surface of described passenger cabin kinematic mount frame 5, and lower end is hinged with the lower end inside face of described passenger cabin kinematic mount frame 5, thus described passenger cabin support 3 can circumferentially rotate；
Described second motor is arranged on passenger cabin kinematic mount frame 5, and described second motor 1 drives described passenger cabin support 3 to be rotated；Described Cab body is arranged in described passenger cabin support 3.
Described fixed frame platform 4 includes base supporting part and the longitudinal bracing portion being vertically connected；
Described passenger cabin kinematic mount frame 5 is arranged in described longitudinal bracing portion and is located at the upside of described base supporting part.
Described first control module and/or described second control module use arduino single-chip microcomputer.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, also include display；
Wherein, in described display is arranged on described ground passenger cabin；Described display electrically connects described second control module.
This utility model provide 360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom, described Position and attitude sensor include such as lower sensor in any one or appoint multiple:
-acceleration transducer；
-Position and attitude sensor；
-torque sensor.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, also include crosswind analog, and described crosswind analog electrically connects described second control module, for simulating the wind speed that described unmanned plane is subject to.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, also include body monitoring device and alarm device；
Wherein, described body monitoring device electrically connects described second control module；Described body monitoring device is for the condition detecting simulated flight personnel and the accekeration being subject to, and described condition and the acceleration being subject to is sent to described second control module to set time threshold；
Described alarm device electrically connects described second control module, and when described condition is less than setting threshold value, or the acceleration being subject to is more than when setting threshold value, and described alarm device sends alarm signal；
Described condition includes in heart rate, respiratory frequency and body temperature any one or appoints multiple.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, described passenger cabin support is cage type.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom that this utility model provides, also include photographic head；
Multiple described photographic head are arranged on front end face and the two sides of described unmanned plane；Multiple described photographic head connect described first control module；
The image information of described camera collection is sent by described first control module by described first communication module；Described second control module receives described image information by described second communication module, and then sends described image information to the broadcasting of described display.
This utility model, the system that aircraft and driving cabin the two are originally one, splits into two relatively independent systems.It is used in the driving cabin on ground to manipulate aerial unmanned plane.This utility model obtains true what comes into a driver's at ground driving cabin, mainly wireless image transmission Technology application has been arrived the visual system part in flight simulation cabin.The visual system in flight simulation cabin was all to pass through computer generated image in the past.The weak point of this virtual reality technology, subject matter is to describe the most true to nature to in-plant scene, makes driver carry out decision height by scene and speed is relatively difficult.But along with raising and the expansion of capacity of the operational speed of a computer, the scene of description also will be increasingly finer and smoother, and more and more true to nature, the problems referred to above will progressively have been resolved.
But computer generated image is the what comes into a driver's simulated all the time, even if by the degree of freedom of dynamic cabin simulator cockpit, a kind of real flying feel also can not be built, because vision is main impression.Making a general survey of flight simulation cabin now is to be all the what comes into a driver's part using virtual reality technology to be done boiler-plate by computer generated image mostly.But wireless image transmission technology is widely used in unmanned plane or the model plane flight realizing first person on unmanned plane or model plane already.In addition, wireless image transmission technology is also used in tele-medicine, criminal investigation aspect, and has significant role.
Additionally this utility model unmanned plane simulates mobility and the operation feeling aspect of true aircraft, can coordinate the viewed mobility of what comes into a driver's, or the mobility that body-sensing is felt.And that accomplishes to operate unmanned plane and true aircraft feels close.The flight quality of true aircraft is simulated, the most also without being carried out, because this is confined to unmanned plane itself with unmanned plane.
And this utility model makes emphatically, and unmanned plane and the mobility of true aircraft are similar to operation feeling starts with, from the beginning of flying vehicles control equation.Simplified analysis, from unmanned plane, with angular acceleration, on the one hand this carry out theory analysis with true aircraft.Sum up manipulation unmanned plane voluntarily and manipulate the operation transformation matrices needed between true aircraft.Finally improve, by experimental flight, the credibility that these flying feels are similar again.
Above specific embodiment of the utility model is described.It is to be appreciated that this utility model is not limited to above-mentioned particular implementation, those skilled in the art can make various deformation or amendment within the scope of the claims, and this has no effect on flesh and blood of the present utility model.
Claims (9)
1. a ground passenger cabin, it is characterised in that include that Cab body, elevating movement drive module and left-right rotation to drive module；Described elevating movement drives Cab body described in module drive to carry out elevating movement, and described left-right rotation drives Cab body left-right rotation described in module drive.
Ground the most according to claim 1 passenger cabin, it is characterised in that described elevating movement drives module to include fixed frame platform, the first motor；Described left-right rotation drives module to include passenger cabin kinematic mount frame, the second motor and passenger cabin support；
Described first motor is arranged on described fixed frame platform；On described passenger cabin kinematic mount frame and described fixed frame table-hinges；Described first motor drives described passenger cabin kinematic mount frame to carry out pitch rotation；
The upper end of described passenger cabin support is hinged with the upper end medial surface of described passenger cabin kinematic mount frame, and lower end is hinged with the lower end inside face of described passenger cabin kinematic mount frame, thus described passenger cabin support can circumferentially rotate；
Described second motor is arranged on passenger cabin kinematic mount frame, and described second motor drives described passenger cabin support to be rotated；Described Cab body is arranged in described passenger cabin support.
Ground the most according to claim 2 passenger cabin, it is characterised in that described fixed frame platform includes base supporting part and the longitudinal bracing portion being vertically connected；
Described passenger cabin kinematic mount frame is arranged in described longitudinal bracing portion and is located at the upside of described base supporting part；
Described passenger cabin support is cage type.
4. 360 degree of flight simulation driving cabin simulating sports platforms of a two degrees of freedom, it is characterized in that, ground passenger cabin described in any one of claims 1 to 3, also includes unmanned plane, ground passenger cabin, the first communication module, the second communication module, the first control module and the second control module；
Wherein, described unmanned plane is provided with Position and attitude sensor, the first communication module and the first control module；Described Position and attitude sensor is for measuring the angle of pitch and the left and right swing angle of unmanned plane；Described first control module connects Position and attitude sensor and the first communication module；
Described second control module connects described elevating movement and drives module, described left-right rotation to drive module and the second communication module；
Described first control module is obtained the described angle of pitch and left and right swing angle and is sent by described first communication module；Described second control module receives the described angle of pitch and described left and right swing angle by described second communication module, and then control described elevating movement driving module rotation according to the described angle of pitch, control described left-right rotation according to described left and right swing angle and drive module to rotate；
The passenger cabin kinematic mount frame of described ground passenger cabin is arranged in the longitudinal bracing portion of described ground passenger cabin and is located at the upside of the base supporting part of described ground passenger cabin.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom the most according to claim 4, it is characterised in that described first control module and/or described second control module use arduino single-chip microcomputer.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom the most according to claim 4, it is characterised in that also include display；
Wherein, in described display is arranged on described ground passenger cabin；Described display electrically connects described second control module.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom the most according to claim 4, it is characterised in that described Position and attitude sensor include such as lower sensor in any one or appoint multiple:
-acceleration transducer；
-Position and attitude sensor；
-torque sensor.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom the most according to claim 4, it is characterised in that also include body monitoring device and alarm device；
Wherein, described body monitoring device electrically connects described second control module；Described body monitoring device is for the condition detecting simulated flight personnel and the accekeration being subject to, and described condition and the acceleration being subject to is sent to described second control module to set time threshold；
Described alarm device electrically connects described second control module, and when described condition is less than setting threshold value, or the acceleration being subject to is more than when setting threshold value, and described alarm device sends alarm signal；
Described condition includes in heart rate, respiratory frequency and body temperature any one or appoints multiple.
360 degree of flight simulation driving cabin simulating sports platforms of two degrees of freedom the most according to claim 6, it is characterised in that also include photographic head；
Multiple described photographic head are arranged on front end face and the two sides of described unmanned plane；Multiple described photographic head connect described first control module；
The image information of described camera collection is sent by described first control module by described first communication module；Described second control module receives described image information by described second communication module, and then sends described image information to the broadcasting of described display.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620008466.0U CN205645015U (en) | 2016-01-05 | 2016-01-05 | Ground passenger cabin and two -degree -of -freedom 360 degree flight driving simulation cabin emulation motion platform |
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| CN201620008466.0U CN205645015U (en) | 2016-01-05 | 2016-01-05 | Ground passenger cabin and two -degree -of -freedom 360 degree flight driving simulation cabin emulation motion platform |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107297736A (en) * | 2017-08-18 | 2017-10-27 | 大连大华中天科技有限公司 | four-degree-of-freedom tandem type motion simulation platform |
| WO2018184218A1 (en) * | 2017-04-07 | 2018-10-11 | 深圳市大疆创新科技有限公司 | Control method, processing device, processor, aircraft, and motion sensing system |
-
2016
- 2016-01-05 CN CN201620008466.0U patent/CN205645015U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018184218A1 (en) * | 2017-04-07 | 2018-10-11 | 深圳市大疆创新科技有限公司 | Control method, processing device, processor, aircraft, and motion sensing system |
| CN108885101A (en) * | 2017-04-07 | 2018-11-23 | 深圳市大疆创新科技有限公司 | Control method, processing unit, processor, aircraft and body-sensing system |
| CN108885101B (en) * | 2017-04-07 | 2021-03-19 | 深圳市大疆创新科技有限公司 | Control method, processing device, processor, aircraft and somatosensory system |
| CN107297736A (en) * | 2017-08-18 | 2017-10-27 | 大连大华中天科技有限公司 | four-degree-of-freedom tandem type motion simulation platform |
| CN107297736B (en) * | 2017-08-18 | 2024-04-09 | 大连大华中天科技有限公司 | Four-degree-of-freedom serial motion simulation platform |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161012 Termination date: 20170105 |