CN202632581U - Flight simulation control and experience device based on real air environment - Google Patents
Flight simulation control and experience device based on real air environment Download PDFInfo
- Publication number
- CN202632581U CN202632581U CN 201220245138 CN201220245138U CN202632581U CN 202632581 U CN202632581 U CN 202632581U CN 201220245138 CN201220245138 CN 201220245138 CN 201220245138 U CN201220245138 U CN 201220245138U CN 202632581 U CN202632581 U CN 202632581U
- Authority
- CN
- China
- Prior art keywords
- flight
- wireless
- ground
- passenger cabin
- dummy vehicle
- 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.)
- Expired - Fee Related
Links
Images
Abstract
The utility model discloses a flight simulation control and experience device based on a real air environment. The flight simulation control and experience device based on the real air environment comprises a ground cabin, a base seat is arranged in the ground cabin, an operation cabin is arranged in the base seat through a multiple spindle rotary system in pivoted mode, a seat is fixedly arranged inside the operation cabin, and a display screen and a flight control table are arranged in a position opposite to the seat. A processor, a wireless data transmission device and a wireless image receiver are arranged inside the ground cabin. The aircraft module is provided with a power supply, a power device, an attitude sensing integrated system, an air pressure sensor, a processor, a wire data transmission device and a flight path vector (FPV) wireless aerial photo system. Therefore, information of scene, height and flight attitude of a real model airplane is transmitted into the ground cabin. True feelings of flight of the real model airplane are restored to an operator through the multiple spindle rotary system and the display screen in the ground cabin, and complete true flight vision and motion sensing experience are brought to the operator. Meanwhile, field control is carried out on the real model airplane through the flight control table so as to increase entertainment.
Description
Technical field
The utility model is about operation of a kind of flight simulation and experience apparatus, refers in particular to a kind ofly to control and experience apparatus based on the flight simulation under the true air environment.
Background technology
At present, the flight simulation operation bench has become electromechanical controlling device indispensable in the flight training field, is one of necessaries of airhog's ab initio training; Simultaneously, comparatively simple flight simulation operation bench also is the electronic amusement apparatus of comparatively popularizing in the public recreation industry, generally comes across in the electronic game Room.
Existing a kind of fly simulation training cabin; Be a kind of analog capsule cabin that is placed in ground, this passenger cabin has reduced the driving cabin environment of true aircraft, but has the whole passenger cabin system that moves of multiaxis; And have the control handwheel and a pin rudder of emulation; And the visual system of high-resolution, come the emulation what comes into a driver's through software, and the passenger cabin attitude and the what comes into a driver's picture of ability simulated flight process.The operator can pass through manipulation dish and pin rudder; With operation signal Input Software system; The software systems computing draws aircraft actual physical parameter; And feed back to the operator through the output of image and passenger cabin rotation two parts of signals, experience so that the operator obtains enough drivings, and make next step flight operation.Though this kind fly simulation training cabin can give the airhog preliminary flight training experience and operating experience; But its flight experience all comes from software systems; Do not have hardware model plane coupling; And the what comes into a driver's scene that software systems simulate is too single, lacks the sense of reality, experiences for the abundanter scene on the spot of operator.
And existing another kind is used for the control system of the true model plane of entertainment field, and its operation control terminal has adopted the IPAD that the respective drive program is housed.The operator can control the taking off of true model plane (for example commercially available AR.DRONE) through operation IPAD, turns to, acceleration and deceleration and landing; And on the true model plane camera is installed, can passes the image of outdoor scene back the IPAD terminal.The control system of the true model plane of this kind; Though reduced the true view of model plane place environment fully; And come the control handwheel of simulated aircraft with the gravity gyro functional part of IPAD, but IPAD is a handheld device, the operator mostly operates on it on straight ground; And the actual physical characteristic of model plane can't feed back to the operator, can't bring the gravity of flying body sense and attitude to change experience.
So, can provide a kind of and control and experience apparatus based on the flight simulation under the true air environment, this device can be controlled the taking off of true model plane, turns to, acceleration and deceleration and landing; And pass real scene image back operation control terminal through camera; Can be provided with multiaxis revolution passenger cabin again, and can read the real-time physical parameter of model plane, these actual parameters fed back to passenger cabin produce rotation; Thereby offering the enough flying body senses of operator experiences; So that the operator obtains more flight impression, flying experience, and provides more comprehensively entertainment effect, promptly become the problem that need solve in the industry.
The utility model content
The purpose of the utility model; Promptly provide and a kind ofly control and experience apparatus based on the flight simulation under the true air environment, this device can be controlled true model plane, is provided with the ground passenger cabin again; Can be with the what comes into a driver's of model plane, highly, information such as flight attitude all passes back in the passenger cabin; And in passenger cabin, produce reduction on the spot, bring the operator with the sense of reality of model plane flight, thereby the actual physical characteristic that overcomes model plane in the background technology can't all feed back to operator's defective.
The purpose of above-mentioned the utility model is to be realized by following technical scheme:
The utility model provides a kind of and controls and experience apparatus based on the flight simulation under the true air environment; Dummy vehicle with a ground passenger cabin and a wireless remote control; Wherein this ground passenger cabin is provided with a base and an operational window; Operational window inside is installed with at least one seat, is provided with a display screen and a flight operation bench in the position that this seat is faced; And this dummy vehicle is provided with power supply and propulsion system; This base of this ground passenger cabin is through a multiaxis rotary system this operational window that is pivoted; And also be provided with this multiaxis rotary system gyration of control in this ground passenger cabin and can handle the operation bench that flies and control the information processing device; One sends and receives the wireless data transmission device of wireless signal, and one provides the wireless image receiver in demonstration source for this display screen; This processor is connected with this flight operation bench, multiaxis rotary system and wireless data transmission device circuit respectively; And the dummy vehicle of a wireless remote control, this dummy vehicle is provided with power supply and propulsion system; Also be provided with one in this dummy vehicle and can collect the attitude sensing integrated system of flight attitude information; One can collect the baroceptor of flying height information; One can control these propulsion system and collect the processor of each sensing data; One sends and receives the wireless data transmission device of wireless signal with this ground passenger cabin, and one can true what comes into a driver's signal be returned the ground passenger cabin the wireless system that takes photo by plane; The processor of this dummy vehicle is connected with the wireless data transmission device circuit with these propulsion system, attitude sensing integrated system, baroceptor respectively.
Aforesaid flight simulation is controlled and experience apparatus; This multiaxis rotary system is the diaxon rotary system; And have two horizontal directions, mutually perpendicular turning axle; Each turning axle is provided with drive motor and travel switch, and drive motor inside also is provided with in order to monitor the code-disc of this turning axle position of rotation.
Aforesaid flight simulation is controlled and experience apparatus; This flight operation bench comprises that a controlling aircraft model starts and flame-out start key; One controlling aircraft model pitching and the flight control bar that tilts, and the power push-rod of controlling aircraft model power output size.
Aforesaid flight simulation is controlled and experience apparatus; This wireless system of taking photo by plane comprises that one is arranged at the camera of dummy vehicle head; One is arranged at the wireless image transmitter in the dummy vehicle; And be arranged at this wireless image receiver in the passenger cabin of ground, wherein this camera is connected with the wireless image transmitter circuit.
Aforesaid flight simulation is controlled and experience apparatus, and this dummy vehicle is a helicopter, fixed-wing aircraft or four-axle aircraft.And the propulsion system of this dummy vehicle comprise at least one screw propeller, and drive the drive motor of this screw propeller.
Aforesaid flight simulation is controlled and experience apparatus, and this attitude sensing integrated system is provided with gyro sensor, and magnetoresistive transducer and acceleration transducer in order to proofread and correct this gyro sensor error.
By above technical scheme, the advantage of the utility model is:
Through in dummy vehicle, be provided with attitude sensing integrated system, FPV is wireless take photo by plane system, baroceptor and wireless data transmission device, can be with the what comes into a driver's of true model plane, highly, information such as direction all passes back in the passenger cabin through wireless signal; And through multiaxis rotary system and display screen are set in passenger cabin, the sense of reality of model plane flight are produced on the spot zone of reduction give the operator, bring complete, especially real flying-vision and body sense to experience to the operator;
Simultaneously; The ground passenger cabin is provided with the flight operation bench, can control on the spot true model plane, again operating experience preferably can be provided for operator's flight training; Especially can make the operator under the addition of flying body sense, in time environmental aspect carried out anticipation and feedback; Make the operator obtain very real flight impression and flying experience, and more comprehensively entertainment effect be provided, be training of software simulation flight operation and hand held remote controlled model plane can not compare.
Description of drawings
Fig. 1 is the overall schematic of the utility model.
Fig. 2 is the block diagram of the circuit part of the utility model.
The main element label declaration:
100 ground passenger cabins, 11 bases
12 rotary systems, 121 drive motor
13 operational windows, 14 seats
15 display screens, 16 flight operation bench
17 processors, 18 wireless data transmission devices
200 dummy vehicles, 21 power supplies
22 propulsion system, 221 screw propellers
222 drive motor, 23 attitude sensing integrated systems
231 gyro sensors, 232 magnetoresistive transducers
233 acceleration transducers, 24 baroceptors
25 processors, 26 wireless data transmission devices
27 system's 271 cameras of infinitely taking photo by plane
272 wireless image transmitters, 273 wireless image receivers
Embodiment
For goal of the invention, technological means and the technique effect that makes the utility model has more complete and clearly exposure, below will specify, and please consult accompanying drawing and parts label in the lump.
The utility model provides a kind of and controls and experience apparatus based on the flight simulation under the true air environment, sees also shown in Figure 1ly, consists predominantly of ground passenger cabin 100 and dummy vehicle 200 two parts.
Wherein, this ground passenger cabin 100 is provided with a base 11, and this base 11 is through a multiaxis rotary system 12 operational window 13 that is pivoted, and operational window 13 inside are installed with at least one seat 14, is provided with a display screen 15 and a flight operation bench 16 in the position that this seat 14 is faced; Please consult shown in Figure 2 more in the lump; Also be provided with these multiaxis rotary system 12 gyrations of control in this ground passenger cabin 100 and can handle the operation bench 16 that flies and control information processing device 17; One sends and receives the wireless data transmission device 18 of wireless signal, and one is the wireless image receiver 273 that this display screen 15 provides the demonstration source; This processor 17 is connected with this flight operation bench 16, multiaxis rotary system 12 and wireless data transmission device 18 circuit respectively.
In the preferred embodiment of the utility model; The rotary system 12 of this multiaxis is the rotary system 12 of a diaxon; This rotary system 12 is pivoted with base 11 mutually, and has two horizontal directions, mutually perpendicular turning axle, has pitching then and tilts two degree of freedom; Respectively by two 800W brushless direct-current drive motor 121 drive belts and gear drive operational window 13 and on seat 14 turn round and tilt, thereby can simulate the attitude of dummy vehicle 200.The brshless DC motor governor control characteristics is good; Driving circuit can adopt existing ripe high-power brushless motor-drive circuit; Have the ability burden two to triplet, and have dynamic promptness of certain motion and accuracy, reach the effect of timely tracking aircraft model 200 flight attitudes.Further; The rotating speed of drive motor 121 is driven by it the strict control of the given pulsed frequency of circuit; Brshless DC motor need dispose code-disc (among the figure indicate) and discern the angle information that is turned over, can be so that rotary system 12 rotate accurately or certain angle that tilts, and combine travel switch (indicating among the figure); Guarantee the accuracy and the reliability of the adjustment of operational window 13 attitudes, to obtain good, lasting flight experience.Certainly, the utility model is not limited to this, and having three rotary systems that rotatablely move also should be within the utility model protection domain.
In the preferred embodiment of the utility model; The deviser is designed with a controlling aircraft model 200 and starts and flame-out start key on this flight operation bench 16; 200 pitching of one controlling aircraft model and the flight control bar that tilts; And the power push-rod of a controlling aircraft model 200 power output size (these three parts all are integrated in the operation bench among Fig. 1, indicate separately), bring in controlling basically of realization dummy vehicle 200 with these three functions; Certainly also can comprise alarm keys, voice broadcast operating key or the like modifier key.But the utility model is not as restriction, and the mechanism that any realization terminal is controlled (the for example touch-screen of IPAD in the background technology) all is under the jurisdiction of within the category of this flight operation bench 16.
In the preferred embodiment of the utility model; What display screen 15 adopted is LCD large-area liquid crystal screen; (specifying) in follow-up dummy vehicle 200 parts, and wireless image receiver 273 can receive the what comes into a driver's picture signal, outputting VGA signal is given display screen 15.
With the ground passenger cabin ground that matches, another main member of the utility model is the dummy vehicle 200 of wireless remote control.Dummy vehicle 200 can be helicopter, fixed-wing aircraft or four-axle aircraft, but is not limited to this.The aircraft that the preferred embodiment of the utility model is adopted is the middle-size and small-size four-axle aircraft that a kind of diameter is about 60cm, and its model plane framework and parts are very ripe in the prior art, and this paper will not launch to detail on existing framework.
See also Fig. 1 and Fig. 2, this dummy vehicle 200 is provided with power supply 21 and propulsion system 22; Also be provided with one in this dummy vehicle 200 and can collect the attitude sensing integrated system 23 of flight attitude information; One can collect the baroceptor 24 of flying height information; One can control these propulsion system 22 and collect the processor 25 of each sensing data; One sends and receives the wireless data transmission device 26 of wireless signal with this ground passenger cabin 100, and one can be with the wireless system 27 that takes photo by plane of the FPV that true what comes into a driver's signal returns the ground passenger cabin; The processor 25 of this dummy vehicle 200 is connected with these propulsion system 22, attitude sensing integrated system 23, baroceptor 24 and wireless data transmission device 26 circuit respectively.
In the preferred embodiment of the utility model, power supply 21 adopts the lithium battery group of 11.1V 5200mAh efficiently, and the mu balanced circuit that model plane are provided with can produce 5V voltage and give each electron device and wireless system's 27 power supplies of taking photo by plane of FPV.In the applied four-axle aircraft of present embodiment; Have four screw propellers 221 altogether; Drive respectively by four brushless direct-current drive motor 222; And four drive motor 222 services for this reason of four motor-drive circuits are arranged, these driving circuits all receive the control of the processor 25 on the dummy vehicle 200, with adjustment flight attitude and speed.In the aircraft of other kinds, the number of screw propeller and necessary electromotor thereof is decided by the form that aircraft drives.
In the preferred embodiment of the utility model, this attitude sensing integrated system 23 is provided with gyro sensor 231, and magnetoresistive transducer 232 and acceleration transducer 233 in order to proofread and correct these gyro sensor 231 errors.Be three-axis sensor with upper sensor, can return the physical message of three directions.Passenger cabin 100 has adopted diaxon rotary system 12 and present embodiment is on ground, and this just means that on dummy vehicle 200, the deviser has only gathered the physical data with rotary system 12 corresponding two axles, comes corresponding with above ground portion with this.When ground passenger cabin 100 adopted the design of three rotary systems 12, it was corresponding with it to gather whole three axial physical messages on the dummy vehicle 200.
The flying height of model plane is important indicators, need at every moment be shown to the operator who is positioned at ground, simultaneously to excessive height, cross low need report to the police and program on qualification.Learn that by prior art altitude information generally can be calculated by atmospheric size and obtain, so the equipment of the collection altitude information that the utility model adopted is baroceptor 24.
FPV is wireless, and the system that takes photo by plane also is prior art, and comprises a camera 271, one wireless image transmitters 272 and a wireless image receiver 273 as the one of which.In the preferred embodiment of the utility model, adopted 400P camera 271 to be arranged at the head of dummy vehicle, wireless image transmitter 272 has the wireless output of high frequency of 5.8GHz, and is connected with camera 271 circuit; And this wireless image receiver 273 is arranged in the aforementioned ground passenger cabin 100, and the outdoor scene of will flying is exported to display screen 15.The utility model FPV is wireless, and the system that takes photo by plane adopts the high-speed digital circuit encoding and decoding, can accomplish that minimum what comes into a driver's postpones, and guarantees image real-time property and the stability passed back.
Owing to have a large amount of outsourcing electronics in the structure of aforesaid the utility model, below just the outsourcing device that is used in the preferred embodiment is shown clearly.But the utility model is as limit, can reach the electron device of any model of any manufacturer production of identical function, all should be included in the category of the utility model protection.
Dummy vehicle adopts ATmega16 high-performance single-chip microcomputer as processor, and this single-chip microcomputer is based on 8 CMOS microcontrollers of low-power consumption of the AVR risc architecture of enhancing.Because its advanced instruction set and single clock cycle instruction time, the data throughput of ATmega16 is up to 1MIPS/MHz, thereby can the contradiction of relieving system between power consumption and processing speed, satisfies the model plane demands of applications basically.
The attitude sensing integrated system of dummy vehicle has been chosen three-axis gyroscope sensor L3G4200D, 3-axis acceleration sensor ADXL345, three magnetoresistive transducer HMC5883 with IIC interface and has been connected with single-chip microcomputer, and the flying height aspect has adopted height sensor BMP085 to be connected with single-chip microcomputer; Allow a plurality ofly to be mounted to simultaneously on the bus, effectively reduced homemade size and the weight that flies to control plate PCB printed circuit board (PCB) of deviser from device.Wherein:
The attitude data of aircraft is mainly obtained by gyro sensor L3G4200D; This device is 3 number of axle word gyroscopes that induction structure of employing of STMicw Electronics (ST) release detects three quadrature axially-movables; The user can set whole ranges; Range ability is from ± 250dps to ± 2000dps, and this device provides one 16 bit data output IIC interface, and embedded digital functions such as configurable low pass and Hi-pass filter.Even if passage of time or temperature variation, this device still keeps the output of continous-stable.
HMC5883 is 3 magnetoresistive transducers that Honeywell Inc. releases, and for low the Magnetic Sensor that has a digital interface designs, is applied to such as low-cost compass and magentometry field specially.HMC5883 is surface mounted in the leadless chip carrier (LCC) of 4.0 * a 4.0 * 1.3mm.The utility model adopts magnetoresistive transducer that gyroscope is proofreaied and correct, and prevents the error that long-time integration brings.
That baroceptor uses is the pressure transducer BMP085 of a high precision, super low energy consumption, and its performance is remarkable, and absolute precision is minimum can to reach 0.03hPa, and power consumption is extremely low, has only 3 μ A.BMP085 adopts powerful 8pin pottery leadless chip to carry (LCC) ultra-thin encapsulation, can directly link to each other with various microprocessors through the I2C bus.Pressure limit is at 300～1100hPa (9000 meters～500 meters of height above sea level), and adopts undersized LCC8 encapsulation.
Moreover; The deviser of the utility model has also adopted and has flown to control plate and integrate above processor and various sensor; And be provided with the driving circuit of model plane with brushless electric machine, through the certain procedure algorithm, make it have model plane self stability (prevent air crash, cross the border) and straighforward operation controllability.Its PCB printed circuit board (PCB) adopts military project level sheet material and turmeric technology, not influenced by vibrations, temperature and the corrosion etc. of complex environment.
Two wireless data transmission devices from ground passenger cabin and dummy vehicle; Be to adopt ripe prior art; Its transmission band is a high-frequency band, and belongs to and exempt from the licence frequency range, and need not the expense of paying can use; Commercially available wireless data transmission device commonly used can be provided with nearly 256 communication channels, can satisfy the communication requirement of the utility model fully.
In addition; The isonomic single chip computer AT mega128 of employed processor adopting and ATmega16 in the passenger cabin of ground, this single-chip microcomputer mainly accomplish the processing of the flight attitude data that receive, the processing of flight operation bench input signal and the functions such as control of rotary system.
By the utility model that above technical scheme is formed, its principle of work is following:
Barnyard is settled dummy vehicle in the open; After the operator sits the seat of ground passenger cabin into; At first with the fixing health of safety equipment such as bumper and securing band, then can operate start key, flight control bar and power push-rod on the flight operation bench, these operating rods and button convert operator's action into electric signal; Give the processor in the passenger cabin; Processor is changed it and is encoded, and is resent to wireless data transmission device, and wireless data transmission device is transmitted to dummy vehicle with these information wireless; Wireless data transmission device on the dummy vehicle receives the control command signal from the ground passenger cabin; Its processor that sends on the dummy vehicle is decoded; Be converted into control signal; Control the screw propeller running that four brushless direct-current drive motor are driven thus, and can make aircraft complete operation person's exercises instruction.And the concrete drive manner of screw propeller flies flying in the device models treated device and controls algorithm decision by being built in, and this algorithm can be accomplished by the calculating to brushless direct-current drive motor operating parameters of the telecommand of the ground passenger cabin that receives.
And each sensor of dummy vehicle receives flight attitude and elevation information; Be converted into electric signal; And deliver to the processor of dummy vehicle, after processor is handled these flight attitudes and elevation information and encoded, pass to wireless data transmission device and be transmitted to the ground passenger cabin; Wireless data transmission device on the passenger cabin of ground receives wireless messages; Send it processor of ground passenger cabin to; Processor is converted into the electric signal of control motor-drive circuit, finally controls the motion of multiaxis rotary system, and flight attitude is directly fed back to the operator with body sensing mode.
Simultaneously, also be provided with the wireless system that takes photo by plane of FPV on the dummy vehicle, can read true what comes into a driver's image from the camera of this system; The image information that it collects; Need not to transfer to processor, but by wireless image transmitter direct coding and launch, finally receive, gather by the wireless image receiver that is installed in the passenger cabin of ground; And in display screen, carry out video picture, to offer the real flying-vision of operator.And the image transmission signals antijamming capability of high frequency is strong, and real-time is high, and the clear nothing of picture is detained.Bring the operator better visual experience.
The above act is merely the schematic part embodiment of the utility model; It is not scope in order to restriction the utility model; Any those skilled in the art; Equivalent variations of under the prerequisite of design that does not break away from the utility model and principle, having done and modification all should be included within this patent protection domain.
Claims (6)
1. control and experience apparatus based on the flight simulation under the true air environment for one kind; Dummy vehicle with a ground passenger cabin and a wireless remote control; Wherein this ground passenger cabin is provided with a base and an operational window; Operational window inside is installed with at least one seat, is provided with a display screen and a flight operation bench in the position that this seat is faced; And this dummy vehicle is provided with power supply and propulsion system, it is characterized in that:
This base of this ground passenger cabin is through a multiaxis rotary system this operational window that is pivoted; And also be provided with this multiaxis rotary system gyration of control in this ground passenger cabin and can handle the operation bench that flies and control the information processing device; One sends and receives the wireless data transmission device of wireless signal, and one provides the wireless image receiver in demonstration source for this display screen; This processor is connected with this flight operation bench, multiaxis rotary system and wireless data transmission device circuit respectively;
Also be provided with one in this dummy vehicle and can collect the attitude sensing integrated system of flight attitude information; One can collect the baroceptor of flying height information; One can control these propulsion system and collect the processor of each sensing data; One sends and receives the wireless data transmission device of wireless signal with this ground passenger cabin, and one can true what comes into a driver's signal be returned the ground passenger cabin the wireless system that takes photo by plane; The processor of this dummy vehicle is connected with the wireless data transmission device circuit with these propulsion system, attitude sensing integrated system, baroceptor respectively.
2. flight simulation according to claim 1 is controlled and experience apparatus; It is characterized in that; This multiaxis rotary system is the diaxon rotary system; And have two horizontal directions, mutually perpendicular turning axle, each turning axle is provided with drive motor and travel switch, and drive motor inside also is provided with in order to monitor the code-disc of this turning axle position of rotation.
3. flight simulation according to claim 1 is controlled and experience apparatus; It is characterized in that; This flight operation bench comprises that the controlling aircraft model starts and flame-out start key; One controlling aircraft model pitching and the flight control bar that tilts, and the power push-rod of controlling aircraft model power output size.
4. flight simulation according to claim 1 is controlled and experience apparatus; It is characterized in that; This wireless system of taking photo by plane comprises that one is arranged at the camera of dummy vehicle head; One is arranged at the wireless image transmitter in the dummy vehicle, and is arranged at this wireless image receiver in the passenger cabin of ground, and wherein this camera is connected with the wireless image transmitter circuit.
5. flight simulation according to claim 1 is controlled and experience apparatus; It is characterized in that; This dummy vehicle is a helicopter, fixed-wing aircraft or four-axle aircraft, and the propulsion system of this dummy vehicle comprise at least one screw propeller, and drives the drive motor of this screw propeller.
6. flight simulation according to claim 1 is controlled and experience apparatus, it is characterized in that, this attitude sensing integrated system is provided with gyro sensor, and magnetoresistive transducer and acceleration transducer in order to proofread and correct this gyro sensor error.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220245138 CN202632581U (en) | 2012-05-28 | 2012-05-28 | Flight simulation control and experience device based on real air environment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220245138 CN202632581U (en) | 2012-05-28 | 2012-05-28 | Flight simulation control and experience device based on real air environment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202632581U true CN202632581U (en) | 2012-12-26 |
Family
ID=47385749
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220245138 Expired - Fee Related CN202632581U (en) | 2012-05-28 | 2012-05-28 | Flight simulation control and experience device based on real air environment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202632581U (en) |
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103170141A (en) * | 2013-03-13 | 2013-06-26 | 西安大地测绘工程有限责任公司 | Unmanned aerial vehicle sightseeing flight experience system |
| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN104217622A (en) * | 2014-08-29 | 2014-12-17 | 喻明 | Simulation aircraft and system thereof |
| CN104269085A (en) * | 2014-09-23 | 2015-01-07 | 内蒙古空港航空地面服务有限公司 | Movable simulation aircraft |
| CN104407607A (en) * | 2014-10-15 | 2015-03-11 | 天津全华时代航天科技发展有限公司 | Unmanned aerial vehicle first-person perspective control system |
| CN104464440A (en) * | 2014-12-19 | 2015-03-25 | 上海电机学院 | Wingsuit flight simulator |
| CN104503257A (en) * | 2014-11-04 | 2015-04-08 | 中国人民解放军海军工程大学 | Scene simulation anti-corona system and method |
| CN104714552A (en) * | 2015-03-11 | 2015-06-17 | 郑州航空工业管理学院 | Four-rotor aircraft based on mobile phone real-time monitoring |
| CN105185189A (en) * | 2015-10-16 | 2015-12-23 | 上海电机学院 | Flight simulation platform |
| CN105388906A (en) * | 2015-11-30 | 2016-03-09 | 无锡觅睿恪科技有限公司 | Height detection remote control for unmanned aerial vehicle (UAV) |
| CN105391984A (en) * | 2015-12-05 | 2016-03-09 | 谭圆圆 | UAV (Unmanned Aerial Vehicle) driving experience system and method |
| CN105489083A (en) * | 2016-01-05 | 2016-04-13 | 上海交通大学 | Two-degree-of-freedom 360-degree flight simulation cockpit simulation motion platform |
| CN105549618A (en) * | 2015-03-18 | 2016-05-04 | 刘建平 | Real-scene interactive control system |
| CN105791754A (en) * | 2015-05-07 | 2016-07-20 | 寺坂立 | Aircraft remote control system |
| CN106227231A (en) * | 2016-07-15 | 2016-12-14 | 深圳奥比中光科技有限公司 | The control method of unmanned plane, body feeling interaction device and unmanned plane |
| CN106611524A (en) * | 2015-10-26 | 2017-05-03 | 冯介川 | A reality control simulation system |
| CN106856073A (en) * | 2017-03-22 | 2017-06-16 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special simulation opportunity of combat model of teenager's research in defense-related science and technology |
| CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
| CN109126119A (en) * | 2018-11-01 | 2019-01-04 | 广州翼凌峰动漫科技有限公司 | A kind of device of playing based on augmented reality |
| CN110083172A (en) * | 2019-05-21 | 2019-08-02 | 郭远芳 | A kind of unmanned vehicle control system |
| CN110404269A (en) * | 2019-09-11 | 2019-11-05 | 张春宇 | A kind of aircraft simulation experience apparatus |
| CN110520918A (en) * | 2017-05-22 | 2019-11-29 | 亚历山大·尤利耶维奇·贝兰基 | Spacecraft flight simulator |
| CN110825102A (en) * | 2018-08-10 | 2020-02-21 | 宝沃汽车（中国）有限公司 | Method and device for controlling unmanned aerial vehicle based on vehicle seat, storage medium and vehicle |
| CN111260992A (en) * | 2018-11-30 | 2020-06-09 | 王振兴 | Simulation flight system and simulation flight method of rotor wing |
| CN112947510A (en) * | 2014-09-30 | 2021-06-11 | 深圳市大疆创新科技有限公司 | System and method for flight simulation |
| CN112987705A (en) * | 2021-03-02 | 2021-06-18 | 北京航空航天大学 | Verification system of automatic airplane sliding running-away technology based on 5G transmission |
| CN113050669A (en) * | 2017-04-07 | 2021-06-29 | 深圳市大疆创新科技有限公司 | Control method, processing device, processor, aircraft and somatosensory system |
-
2012
- 2012-05-28 CN CN 201220245138 patent/CN202632581U/en not_active Expired - Fee Related
Cited By (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103170141A (en) * | 2013-03-13 | 2013-06-26 | 西安大地测绘工程有限责任公司 | Unmanned aerial vehicle sightseeing flight experience system |
| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN103886782B (en) * | 2014-04-09 | 2016-06-01 | 陈京波 | A kind of 360 degree of omnidirectionals overload type of flight simulator |
| CN104217622A (en) * | 2014-08-29 | 2014-12-17 | 喻明 | Simulation aircraft and system thereof |
| CN104269085A (en) * | 2014-09-23 | 2015-01-07 | 内蒙古空港航空地面服务有限公司 | Movable simulation aircraft |
| CN112947510A (en) * | 2014-09-30 | 2021-06-11 | 深圳市大疆创新科技有限公司 | System and method for flight simulation |
| CN104407607A (en) * | 2014-10-15 | 2015-03-11 | 天津全华时代航天科技发展有限公司 | Unmanned aerial vehicle first-person perspective control system |
| CN104503257A (en) * | 2014-11-04 | 2015-04-08 | 中国人民解放军海军工程大学 | Scene simulation anti-corona system and method |
| CN104503257B (en) * | 2014-11-04 | 2017-07-07 | 中国人民解放军海军工程大学 | The anti-corona system and method for vision simulation |
| CN104464440A (en) * | 2014-12-19 | 2015-03-25 | 上海电机学院 | Wingsuit flight simulator |
| CN104714552A (en) * | 2015-03-11 | 2015-06-17 | 郑州航空工业管理学院 | Four-rotor aircraft based on mobile phone real-time monitoring |
| CN105549618A (en) * | 2015-03-18 | 2016-05-04 | 刘建平 | Real-scene interactive control system |
| CN105791754B (en) * | 2015-05-07 | 2018-10-30 | 寺坂立 | The joystick system of aircraft |
| CN105791754A (en) * | 2015-05-07 | 2016-07-20 | 寺坂立 | Aircraft remote control system |
| CN105185189A (en) * | 2015-10-16 | 2015-12-23 | 上海电机学院 | Flight simulation platform |
| CN106611524A (en) * | 2015-10-26 | 2017-05-03 | 冯介川 | A reality control simulation system |
| TWI584240B (en) * | 2015-10-26 | 2017-05-21 | 馮介川 | Reality operating emulation system |
| CN105388906A (en) * | 2015-11-30 | 2016-03-09 | 无锡觅睿恪科技有限公司 | Height detection remote control for unmanned aerial vehicle (UAV) |
| CN105391984A (en) * | 2015-12-05 | 2016-03-09 | 谭圆圆 | UAV (Unmanned Aerial Vehicle) driving experience system and method |
| CN105489083A (en) * | 2016-01-05 | 2016-04-13 | 上海交通大学 | Two-degree-of-freedom 360-degree flight simulation cockpit simulation motion platform |
| CN106227231A (en) * | 2016-07-15 | 2016-12-14 | 深圳奥比中光科技有限公司 | The control method of unmanned plane, body feeling interaction device and unmanned plane |
| CN106856073A (en) * | 2017-03-22 | 2017-06-16 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special simulation opportunity of combat model of teenager's research in defense-related science and technology |
| CN113050669A (en) * | 2017-04-07 | 2021-06-29 | 深圳市大疆创新科技有限公司 | Control method, processing device, processor, aircraft and somatosensory system |
| CN110520918A (en) * | 2017-05-22 | 2019-11-29 | 亚历山大·尤利耶维奇·贝兰基 | Spacecraft flight simulator |
| CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
| CN107396058B (en) * | 2017-08-23 | 2020-05-15 | 芜湖超源力工业设计有限公司 | Special flight simulation training monitoring device for aerospace |
| CN110825102A (en) * | 2018-08-10 | 2020-02-21 | 宝沃汽车（中国）有限公司 | Method and device for controlling unmanned aerial vehicle based on vehicle seat, storage medium and vehicle |
| CN109126119A (en) * | 2018-11-01 | 2019-01-04 | 广州翼凌峰动漫科技有限公司 | A kind of device of playing based on augmented reality |
| CN111260992A (en) * | 2018-11-30 | 2020-06-09 | 王振兴 | Simulation flight system and simulation flight method of rotor wing |
| CN110083172A (en) * | 2019-05-21 | 2019-08-02 | 郭远芳 | A kind of unmanned vehicle control system |
| CN110083172B (en) * | 2019-05-21 | 2022-02-11 | 郭远芳 | Unmanned vehicles control system |
| CN110404269A (en) * | 2019-09-11 | 2019-11-05 | 张春宇 | A kind of aircraft simulation experience apparatus |
| CN112987705A (en) * | 2021-03-02 | 2021-06-18 | 北京航空航天大学 | Verification system of automatic airplane sliding running-away technology based on 5G transmission |
| CN112987705B (en) * | 2021-03-02 | 2022-06-28 | 北京航空航天大学 | Verification system of airplane automatic sliding running and driving-off technology based on 5G transmission |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202632581U (en) | Flight simulation control and experience device based on real air environment | |
| US11276325B2 (en) | Systems and methods for flight simulation | |
| US11204611B2 (en) | Assisted takeoff | |
| CN201604796U (en) | Intelligent aerial photography unmanned aerial vehicle | |
| KR20130081260A (en) | Apparatus for controlling unmanned vehicle and unmanned vehicle having the said apparatus | |
| US9493237B1 (en) | Remote control system for aircraft | |
| CN102566441A (en) | Visual simulation test system for unmanned aerial vehicle (UAV) | |
| CN106843276A (en) | A kind of tilting rotor wing unmanned aerial vehicle control system | |
| KR20180026280A (en) | Drone trainer | |
| CN106292713A (en) | A kind of multi-rotor aerocraft control system | |
| US9776730B1 (en) | Independently operable flight data capture and transmission device | |
| CN201978498U (en) | Multifunctional experiential remote control system | |
| Rawashdeh et al. | Microraptor: A low-cost autonomous quadrotor system | |
| CN106809379A (en) | A kind of unmanned aerial vehicle | |
| Yang et al. | Implementation of an autonomous surveillance quadrotor system | |
| O'Connor | Developing a Multirotor UAV Platform to Carry Out Research Into Autonomous Behaviours, Using On-board Image Processing Techniques (BE Thesis), Faculty of Engineering | |
| CN112201115A (en) | Flight simulator | |
| CN106686258A (en) | Control method and system of detachable unmanned aerial vehicle | |
| KR100436086B1 (en) | A Radio Control Helicopter Tranining Simulation System | |
| CN105988476A (en) | Search and rescue system based on six-axis aircraft, and control method thereof | |
| CN217034953U (en) | Teaching training device for simulating real flight attitude of airplane | |
| CN213844443U (en) | Flight simulator | |
| CN210131384U (en) | Toy aircraft | |
| CN211810229U (en) | Binary channels control four shaft air vehicle | |
| TWI786978B (en) | System for controlling powerless fixed-wing airplane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121226 Termination date: 20150528 |
|
| EXPY | Termination of patent right or utility model |