CN204208301U - A kind of aerial image harvester - Google Patents
A kind of aerial image harvester Download PDFInfo
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- CN204208301U CN204208301U CN201420713832.3U CN201420713832U CN204208301U CN 204208301 U CN204208301 U CN 204208301U CN 201420713832 U CN201420713832 U CN 201420713832U CN 204208301 U CN204208301 U CN 204208301U
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Abstract
The utility model discloses a kind of aerial image harvester, belong to field of picture communication, comprise: aeromodelling airplane, described aeromodelling airplane comprises fuselage, described waist is provided with wing, described afterbody is provided with empennage, described wing and empennage are equipped with steering wheel, described afterbody is also provided with steering wheel and screw, the power transmission shaft of described motor is connected with the blade root of described screw, described belly is provided with image acquisition device, described fuselage is provided with wireless device and processor, described wireless device is all connected with described processor with described image acquisition device, described processor is connected with described steering wheel and described motor respectively.The utility model provides a kind of aerial image harvester, effectively to reduce the cost of the aerial survey unmanned plane of IMAQ in prior art.
Description
Technical field
The utility model relates to field of picture communication, in particular to a kind of aerial image harvester.
Background technology
Aerophotogrammetry technology, as one of the Liang great branch of Spatial Information Technology system, has important application in Surveying and Mapping Industry.Traditional aerial equipment weight, carrier aircraft is comparatively large, uses underaction, higher to personnel requirement, so there is no to obtain large area and popularizes.Along with the progress of science and technology, unmanned plane progressively spreads to civilian industry from military field.Compare traditional air-mapping aircraft, unmanned plane possess with low cost, fly that control personal security, flight expense are lower, maneuverability, functional diversities, task development rate quick and the advantage such as over the horizon automatic Pilot.
But inventor finds under study for action, the aerial survey unmanned plane function of prior art is too much, comprising modules too much, for the user only aerial survey unmanned plane being used for IMAQ, and high cost.
Utility model content
The purpose of this utility model is to provide a kind of aerial image harvester, effectively to reduce the cost for the aerial survey unmanned plane of IMAQ in prior art.
First aspect, a kind of aerial image harvester that the utility model provides, comprise: aeromodelling airplane, described aeromodelling airplane comprises fuselage, described waist is provided with wing, described afterbody is provided with empennage, described afterbody is also provided with motor and screw, the power transmission shaft of described motor is connected with the blade root of described screw, described belly is provided with aerial image harvester, described fuselage is provided with wireless device and processor, and described wireless device is all connected with described processor with described image acquisition device.
In conjunction with first aspect, the utility model embodiment still provides the first possibility embodiment of first aspect, wherein, the belly of described fuselage is provided with groove, described groove is provided with baffle plate, described image acquisition device is positioned at described groove, and described in described baffle, image acquisition device is by landing in described groove.
In conjunction with the first possibility embodiment of first aspect, the utility model embodiment still provides the second possibility embodiment of first aspect, and wherein, described baffle plate and described groove removably connect.
In conjunction with first aspect, the utility model embodiment still provides the third possibility embodiment of first aspect, wherein, described fuselage is also provided with steering wheel, described steering wheel comprises the first steering wheel and the second steering wheel, described first steering wheel is connected with described wing, and described second steering wheel is connected with described empennage, and described first steering wheel is all connected with described processor with described second steering wheel.
In conjunction with the third possibility embodiment of first aspect, the utility model embodiment still provides the 4th kind of possibility embodiment of first aspect, wherein, described fuselage is provided with shutter control apparatus, described processor is connected with described shutter control apparatus, and described shutter control apparatus is connected with described image acquisition device.
In conjunction with first aspect, the utility model embodiment still provides the 5th kind of possibility embodiment of first aspect, and wherein, described fuselage is also provided with pitot meter, and described pitot meter is arranged on the head of described fuselage, and described pitot meter is connected with described processor.
In conjunction with first aspect, the utility model embodiment still provides the 6th kind of possibility embodiment of first aspect, and wherein, described fuselage is also provided with positioning navigation device, and described positioning navigation device is connected with described processor.
In conjunction with first aspect, the utility model embodiment still provides the 7th kind of possibility embodiment of first aspect, and wherein, described fuselage is also provided with measurement of flying posture device, and described measurement of flying posture device is connected with described processor.
In conjunction with first aspect, the utility model embodiment still provides the 8th kind of possibility embodiment of first aspect, and wherein, described empennage is rudder-vator.
In conjunction with the 4th kind of embodiment of first aspect, the utility model embodiment still provides the 9th kind of possibility embodiment of first aspect, wherein, described fuselage is also provided with electron speed regulator, described fuselage is also provided with battery and electron speed regulator, described battery is connected with described processor, and described processor is connected with described electron speed regulator, and described electron speed regulator is connected with described motor and described steering wheel.
The technique effect that the utility model realizes: a kind of aerial image harvester that the utility model embodiment provides, described image acquisition device is arranged on the belly of described aeromodelling airplane, the rotation of screw described in described Electric Machine Control, the instruction of described wireless device satellite receiver, described processor controls described image acquisition device and completes shooting task.The aerial survey unmanned plane too much with module with the function of prior art is compared, and it is using aeromodelling airplane as carrier aircraft, compared with the air-mapping aircraft of prior art, significantly reduces cost; It is assembled into described aeromodelling airplane by for the image acquisition device of IMAQ and transmission, processor and wireless device, has simplified function and module, has significantly reduced cost.
Further, a kind of aerial image harvester that the utility model embodiment provides, can also change different image acquisition devices by described groove with from the baffle plate that described groove removably connects.Described image acquisition device is arranged in described groove, described in described baffle, image acquisition device is by landing in described groove, when described image acquisition device changed by needs, pulls down described baffle plate, change described image acquisition device, more described baffle plate is reinstalled on described groove.
Further, a kind of aerial image harvester that the utility model embodiment provides, wing described in described first servos control, and then control the rolling of described aeromodelling airplane; Empennage described in described second servos control, and then control the pitching of described aeromodelling airplane.When described first steering wheel and described second steering wheel arbitrary breaks down, the steering wheel that processor automatic switchover another one does not break down makes described aerial image harvester force-land, and reduces the proportion of goods damageds of described device.
Further, a kind of aerial image harvester that the utility model embodiment provides, startup and the closedown of the taking module of described image acquisition device is controlled by shutter control apparatus, by the startup of image acquisition device described in described wireless device Long-distance Control, the program also can preset by described processor starts described image acquisition device.
Further, a kind of aerial image harvester that the utility model embodiment provides, the cost of a kind of aerial image harvester of the utility model embodiment effectively can also be reduced by described electric steering engine, in addition, the fuel power engine of prior art from great, vibrations are large and comparatively large on the impact of aircraft and IMAQ, and the cost of later maintenance is high, and the motor of the utility model embodiment, effectively overcome fuel power engine from great, that vibrations are large and maintenance cost is high shortcoming.
Further, a kind of aerial image harvester that the utility model embodiment provides, can also measure the speed of described aeromodelling airplane by pitot meter, and successively by after described processor and described wireless device, be sent to earth station's part, start the function of monitoring in real time.
Further, a kind of aerial image harvester that the utility model embodiment provides, the position of described aeromodelling airplane can also be obtained by positioning navigation device, and according to earth station's instruction partly, the position in automatic location tasks place, guides described aerial image harvester to fly to task place by described positioning navigation device by processor.
Other feature and advantage of the present utility model are set forth at description subsequently, and, partly become apparent from description, or understand by implementing the utility model embodiment two.The purpose of this utility model and other advantages realize by structure specifically noted in write description, claims and accompanying drawing and obtain.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme of the embodiment of the present invention, be briefly described to the accompanying drawing used required in embodiment below, be to be understood that, the following drawings illustrate only some embodiment of the present invention, therefore the restriction to scope should be counted as, for those of ordinary skill in the art, under the prerequisite not paying creative work, other relevant accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 shows the side-looking structure chart of a kind of aerial image harvester that the utility model embodiment provides;
Fig. 2 shows the plan structure figure of a kind of aerial image harvester that the utility model embodiment provides;
Fig. 3 shows the partial enlarged drawing of the image acquisition device of a kind of aerial image harvester that the utility model embodiment provides;
Fig. 4 shows the circuit theory diagrams of a kind of aerial image harvester that the utility model embodiment provides.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, carry out clear, complete description to the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
The utility model embodiment is applied to aerophotogrammetry system, and described aerophotogrammetry system comprises aerial image harvester and earth station, and described earth station is data processing centre, can be a server group also can be a data processor.
At present, aerophotogrammetry technology, as one of the Liang great branch of Spatial Information Technology system, has important application in Surveying and Mapping Industry.Traditional aerial equipment weight, carrier aircraft is comparatively large, uses underaction, higher to personnel requirement, so there is no to obtain large area and popularizes.Along with the progress of science and technology, unmanned plane progressively spreads to civilian industry from military field.Compare traditional air-mapping aircraft, unmanned plane possess with low cost, fly that control personal security, flight expense are lower, maneuverability, functional diversities, task development rate quick and the advantage such as over the horizon automatic Pilot.
But inventor finds under study for action, the aerial survey unmanned plane function of prior art is too much, comprising modules too much, for the user only aerial survey unmanned plane being used for IMAQ, and high cost.
A kind of aerial image harvester of thering is provided of the utility model embodiment as shown in Figure 1, comprise: aeromodelling airplane, described aeromodelling airplane comprises fuselage 100, wing 101 is provided with in the middle part of described fuselage 100, described wing 101 removably connects with described fuselage 100, be easy to carry, described fuselage 100 afterbody is provided with empennage 102, described fuselage 100 is the cavity of inner hollow, described fuselage 100 afterbody is provided with screw 103, the inside at described fuselage 100 afterbody place is provided with motor 105, the power transmission shaft of described motor 105 is connected with the blade root of described screw 103, described fuselage 100 belly is provided with image acquisition device 109, the head of described fuselage 100 is provided with wireless device 106, described fuselage 100 inside is provided with processor 108, described wireless device 106 is all connected with described processor 108 with described image acquisition device 109.As shown in Figure 4, described fuselage is also provided with electron speed regulator 200, and described processor 108 is connected with described electron speed regulator 200, and described electron speed regulator 200 is connected with described motor 105.
Described wireless device 106 can receive remote control signal and be input in described processor 108, and described processor 108 controls described electron speed regulator 200 according to described remote control signal.
Also steering wheel is installed in described fuselage 100, described steering wheel comprises the first steering wheel and the second steering wheel, described first steering wheel is connected with described wing, for controlling the rolling of aeromodelling airplane by controlling wing, described second steering wheel is connected with described empennage, and for controlling the pitching of aeromodelling airplane by controlling empennage, steering wheel is also known as servomotor, steering wheel forms primarily of following components, steering wheel, train of reduction gears, position feedback potentiometer, direct current generator, control circuit etc.Described electron speed regulator 200 is connected with the control circuit in described motor 105, and then controls rotation direction and the speed of motor in described motor 105, and then controls the action of wing and empennage.
Described image acquisition device 109 is for gathering ground image information.Described processor 108 can also control startup and the stopping of described image acquisition device 109, specific implementation is: be also provided with shutter control apparatus in described fuselage 100, arrange lead-in wire to be connected with described shutter control apparatus at the shutter release place of described image acquisition device 109, described shutter control apparatus is connected with described processor.In use, described processor controls startup and the stopping of the shutter of described image acquisition device by described shutter control apparatus.After can receiving remote signal by described wireless device, start the shutter of described image acquisition device according to this remote signal, also automatically can start the shutter of described image acquisition device according to the assignment instructions preset in processor.
In addition, described fuselage is provided with positioning navigation device 110, the position of described aeromodelling airplane is obtained by positioning navigation device 110, and according to earth station's instruction partly, by the position in the automatic location tasks place of described processor 108, described aerial image harvester is guided to fly to task place by described positioning navigation device 110 by described processor 108.Described positioning navigation device 110 is GPS navigator, therefore, the aerial image harvester that the utility model embodiment provides can either, by aeromodelling airplane lifting and flight described in remote controller Non-follow control, also can make described aeromodelling airplane automatically fly by positioning navigation device 110 and described processor 108.
In addition, described fuselage 100 is also provided with pitot meter 107, and described pitot meter 107 is arranged on the head of described fuselage 100, can be measured the speed of described aeromodelling airplane by pitot meter 107.
In addition, described fuselage 100 is also provided with measurement of flying posture device, and for measuring the flight attitude of aeromodelling airplane, the measurement of flying posture device of the utility model embodiment is attitude gyro.
Moreover in the utility model embodiment, described image acquisition device 109 is civilian micro-one camera, micro-one camera of the NEX of Sony series or α 7 series can be adopted particularly.The size of described image acquisition device 109 is mated with described groove 113 size.In addition, can select suitable micro-one camera or other cameras flexibly according to the acquisition precision of actual required by task of taking photo by plane, the utility model embodiment only enumerates an embodiment, does not limit the concrete model of described image acquisition device 109.
In specific implementation process, first by controlling and the matching used remote controller of described aeromodelling airplane, control described aeromodelling airplane to take off, after described aeromodelling airplane flies to specified altitude assignment, start automatic offline mode, described aeromodelling airplane flies behind appointed place automatically, and described processor starts the shutter of described image acquisition device by described shutter control apparatus, the image of described image acquisition device shooting appointed place, and be stored in described image acquisition device.
In addition, described positioning navigation device 110, described pitot meter 107, described measurement of flying posture device can the state of flights of Real-Time Monitoring aeromodelling airplane, the information such as such as flight attitude, flying speed and location point, when state of flight information collected by described processor, be sent to earth station by wireless device, earth station can obtain the state of flight of aeromodelling airplane in real time.
In addition, the instruction that described wireless device satellite receiver is launched, is controlled the duty of described first steering wheel, described second steering wheel and described motor by described processor, and then the flight locations controlling the flight attitude of aeromodelling airplane, flying speed and specify.
Therefore, a kind of aerial image harvester that the utility model embodiment provides, described image acquisition device is arranged on the belly of described aeromodelling airplane, control described steering wheel by described processor again and then control the flight of described aeromodelling airplane, and by described processor control described image acquisition device carry out IMAQ realize aerial image gather function.The aerial survey unmanned plane too much with module with the function of prior art is compared, it is using aeromodelling airplane as carrier aircraft, with existing civil camera for image acquisition device, be connected by the processor of shutter control apparatus with described aeromodelling airplane, realize the function of Aerial photography, compared with the air-mapping aircraft of prior art, significantly reduce cost; It is assembled into described aeromodelling airplane by for the image acquisition device of IMAQ and transmission, processor and wireless device, has simplified function and module, has significantly reduced cost.
In addition, in the utility model embodiment, described aeromodelling airplane is the prompt power claws of a hawk in sky, can provide larger loading capacity and better stability.
In addition, as shown in Figure 2, described empennage is rudder-vator, adopts rudder-vator can effectively reduce the impact of empennage rudder face by wing air-flow, strengthens stability.
In addition, the fuel power engine of prior art from great, vibrations are large and comparatively large on the impact of aircraft and IMAQ, and the cost of later maintenance is high, and the motor of the utility model embodiment, effectively overcome fuel power engine from great, maintenance cost is high and shake large shortcoming.Described motor, concrete model is KV680, and this motor power is sufficient, and operating efficiency is high.Described fuselage is provided with battery 111, and described battery 111 is powered for the electrical equipment of the aerial image harvester that the utility model embodiment provides.Described battery 111 is 10000mA lithium battery.
In addition, as shown in Figure 3, the belly of the fuselage 100 of the aeromodelling airplane of the aerial image harvester that the utility model embodiment provides is provided with groove 113, described image acquisition device 109 is arranged in described groove 113, as shown in Figure 3, described groove 113 is rectangular recess, the width of described groove 113 is consistent with the length direction of described fuselage 100, the two ends of the length direction of described groove 113 are equipped with baffle plate 104, described baffle plate 104 stops that described image acquisition device 109 is by landing in described groove 113, ensure when described aeromodelling airplane flight, described image acquisition device 109 firmly can be positioned at the belly of described fuselage 100.
In addition, described baffle plate 104 removably connects with described groove 113, particularly, described baffle plate 104 and described groove 113 snapping, when described image acquisition device 109 is positioned at described groove 113, described baffle plate 104 contacts with the position of depositing battery with the handle place of described image acquisition device 109, stops that described image acquisition device 109 is by landing in described groove 113, and makes the camera lens of described image acquisition device 109 expose described groove 113.
As shown in Figure 4, the circuit theory diagrams of a kind of image collecting device that the utility model provides, comprise: shutter control apparatus 204, image acquisition device 109, wireless device 106, battery 111, pitot meter 107, positioning navigation device 110, electron speed regulator 200, motor 105, processor 108, first steering wheel 201, second steering wheel 202, remote controller 203 and earth station, described earth station is in ground service, send and Received signal strength for the long-range aerial image harvester provided to the utility model embodiment, described remote controller 203 sends signals to described processor for long-range, and then the taking off of remote controlled model airplane.Described battery 111 is for powering for all electrical equipments in aeromodelling airplane, described electron speed regulator 200, on the one hand for described motor 105, first steering wheel 201 and the second steering wheel 202 provide voltage, exports control signal on the other hand and controls described motor 105, first steering wheel 201 and the second steering wheel 202.
The shutter of described image acquisition device 109 is physical button, the shutter pin of a triggering signal to described image acquisition device 109 is produced in time pressing physical button, the present embodiment, draw a wire by the shutter pin of described image acquisition device 109 to be connected with the output of described shutter control apparatus 204, the input of described shutter control apparatus 204 is connected with described processor 108.
Therefore, in the utility model embodiment, described positioning navigation device 110 sets the position of spot for photography, described processor 108 to fly appointed place by controlling described first steering wheel 201, second steering wheel 202 and described motor 105 and then controlling aeromodelling airplane, described shutter control apparatus 204 is outputed signal to again by described processor 108, by shutter control apparatus 204 input signal to the shutter pin of described image acquisition device 109, described image acquisition device 109 starts shoot function, the image in shooting task place.
For circuit principle structure figure of the present utility model, and according to shooting mission requirements, relative set is done to the parameter between each device, such as, a correction value is set when aspect shakiness time, such as aircraft turn, steering wheel needs great angle correction, needs an erection rate to make aircraft recover normal very soon when aircraft of having turned points to destination.Compared with the flight control system of the aeromodelling airplane of prior art, do not need to use attitude gyro just can realize the adjustment of the flight attitude of aeromodelling airplane preferably, decrease unnecessary module, reduce further cost.
In addition, the described aerial image harvester that the utility model embodiment provides, is stored the image of shooting by described image acquisition device 109, when aeromodelling airplane returns to ground, takes out the image stored in described image acquisition device 109.The realtime graphic transmitting device of prior art, first encoder is needed image information to be encoded into the information of certain format, in order to avoid rain declines to the decay of signal, also need setting power amplifier, before signal power is amplified, unwanted signal in the picture signal also needing a digital filter filtering to gather, signal after power amplifier amplifies also needs wireless launcher to be transmitted into earth station, therefore the realtime graphic transmitting device of prior art at least needs encoder, wave filter, power amplifier and wireless launcher, so the utility model embodiment compared with prior art, remove unnecessary module, reduce further cost.
Be understandable that, the utility model can be used in numerous general or special purpose computing system environment or configuration.Such as: personal computer, server computer, handheld device or portable set, laptop device, multicomputer system, system, set top box, programmable consumer-elcetronics devices, network PC, minicom, mainframe computer, the DCE comprising above any system or equipment etc. based on microprocessor.
It should be noted that, in this article, the such as relational terms of first and second grades and so on is only used for an entity or operation to separate with another entity or operating space, and not necessarily requires or imply the relation that there is any this reality between these entities or operation or sequentially.And, term " comprises ", " comprising " or its any other variant are intended to contain comprising of nonexcludability, thus make to comprise the process of a series of key element, method, article or equipment and not only comprise those key elements, but also comprise other key elements clearly do not listed, or also comprise by the intrinsic key element of this process, method, article or equipment.When not more restrictions, the key element limited by statement " comprising ... ", and be not precluded within process, method, article or the equipment comprising described key element and also there is other identical element.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. an aerial image harvester, it is characterized in that, comprise: aeromodelling airplane, described aeromodelling airplane comprises fuselage, described waist is provided with wing, described afterbody is provided with empennage, described afterbody is also provided with motor and screw, the power transmission shaft of described motor is connected with the blade root of described screw, described belly is provided with image acquisition device, described fuselage is provided with wireless device and processor, and described wireless device is all connected with described processor with described image acquisition device, and described processor is connected with described motor.
2. aerial image harvester according to claim 1, it is characterized in that, the belly of described fuselage is provided with groove, and described groove is provided with baffle plate, described image acquisition device is positioned at described groove, and described in described baffle, image acquisition device is by landing in described groove.
3. aerial image harvester according to claim 2, is characterized in that, described baffle plate and described groove removably connect.
4. aerial image harvester according to claim 1, it is characterized in that, described fuselage is also provided with steering wheel, described steering wheel comprises the first steering wheel and the second steering wheel, described first steering wheel is connected with described wing, described second steering wheel is connected with described empennage, and described first steering wheel is all connected with described processor with described second steering wheel.
5. aerial image harvester according to claim 1, is characterized in that, described fuselage is provided with shutter control apparatus, and described processor is connected with described shutter control apparatus, and described shutter control apparatus is connected with described image acquisition device.
6. aerial image harvester according to claim 1, is characterized in that, described fuselage is also provided with pitot meter, and described pitot meter is arranged on the head of described fuselage, and described pitot meter is connected with described processor.
7. aerial image harvester according to claim 1, is characterized in that, described fuselage is also provided with positioning navigation device, and described positioning navigation device is connected with described processor.
8. aerial image harvester according to claim 1, is characterized in that, described fuselage is also provided with measurement of flying posture device, and described measurement of flying posture device is connected with described processor.
9. aerial image harvester according to claim 1, is characterized in that, described empennage is rudder-vator.
10. aerial image harvester according to claim 5, it is characterized in that, described fuselage is also provided with battery and electron speed regulator, and described battery is connected with described processor, described processor is connected with described electron speed regulator, and described electron speed regulator is connected with described motor and described steering wheel.
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| CN201420713832.3U CN204208301U (en) | 2014-11-24 | 2014-11-24 | A kind of aerial image harvester |
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| CN201420713832.3U CN204208301U (en) | 2014-11-24 | 2014-11-24 | A kind of aerial image harvester |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105676870A (en) * | 2016-01-18 | 2016-06-15 | 国家基础地理信息中心 | Photo control point information collecting method and system based on unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105676870A (en) * | 2016-01-18 | 2016-06-15 | 国家基础地理信息中心 | Photo control point information collecting method and system based on unmanned plane |
| CN105676870B (en) * | 2016-01-18 | 2018-08-21 | 国家基础地理信息中心 | A kind of photo control point information collecting method and system based on unmanned plane |
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