CN204575195U - Based on illuminometer and the illumination test group of flight location - Google Patents
Based on illuminometer and the illumination test group of flight location Download PDFInfo
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- CN204575195U CN204575195U CN201520196438.1U CN201520196438U CN204575195U CN 204575195 U CN204575195 U CN 204575195U CN 201520196438 U CN201520196438 U CN 201520196438U CN 204575195 U CN204575195 U CN 204575195U
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Abstract
The utility model relates to a kind of illuminometer based on flight location and illumination test group, should based on the illuminometer of flight location by arranging illuminometer and displacement location device on board the aircraft, and controlled by controller, thus more people's Force meansurement can be saved, save time and cost, and accurate positioning, improve measuring accuracy.Form graticule mesh shape measuring point by this illumination test group and can expand test area, realize multiposition and jointly test, contribute to improving the test duration and contributing to cost-saving.
Description
Technical field
The utility model relates to a kind of illuminometer based on flight location and illumination test group.
Background technology
The only energy, also be the indispensable base substances of the mankind, illumination test is then understand perceived light to exist, carry out light effectively utilizing the basic means controlled, purposes is wide and utilize general, usual by illuminometer realization illumination test at present, a kind of wireless illuminometer disclosed in No. 201210390908th, Chinese patent application, it comprises a handheld device and at least one measuring terminals, wirelessly communicate between handheld device and measuring terminals, handheld device sends instructions to measuring terminals, measurement data is sent to handheld device by measuring terminals, when wireless illuminometer only includes a measuring terminals, point-to-point communication protocol is used between handheld device and measuring terminals, when described wireless illuminometer comprises multiple measuring terminals, adopt the communication of multihop network protocol realization.Although this is wireless, illuminometer can realize wireless transmission, when detection, need manually this wireless illuminometer hand-held to operate, measuring point needs mobile after having surveyed, take time and effort, can not test fast.
Utility model content
For solving the problems of the technologies described above, the purpose of this utility model is to provide a kind of illuminometer based on flight location, can save more people's Force meansurement, save time and cost, and accurate positioning, improve measuring accuracy.
A kind of illuminometer based on flight location of the present utility model, comprise aircraft, described aircraft comprises flying body, be arranged on illuminometer on described flying body and displacement location device and controller, described controller is connected with flying body and displacement location device respectively, the position of monitored flying body is also sent to controller by the position of described displacement location device Real-Time Monitoring flying body, the position of the flying body that described controller monitors according to displacement location device controls the moving direction of flying body and/or amount of movement and/or sense of rotation, described illuminometer is connected with described controller and controls it by described controller and starts to detect brightness value, and detected brightness value is sent to controller by described illuminometer.
Further improvement: described flying body is provided with the display circuit be connected with described controller signals to show brightness value and bearing data.
Further improvement: described controller be provided with the enter key/of the bearing data manually inputting required surveyed area or click the gps data of input tracking automatically.
Further improvement: the described illuminometer based on flight location also comprises remote control, and described remote control is connected with controller signals, and controls described controller.
Further improvement: the control zone that described remote control comprises the bearing data for inputting surveyed area and the transceiver be connected with described control zone signal, transmitting and receiving module is provided with in described controller, described transceiver is connected with transmitting and receiving module signal, bearing data is sent to transmitting and receiving module by described transceiver, and brightness value is sent to transceiver by described transmitting and receiving module.
Further improvement: described remote control also comprises viewing area, described viewing area is connected with control zone, transceiver and receives display orientation data and brightness value.
Further improvement: described aircraft is provided with the power supply of powering to illuminometer, displacement location device and controller.
The utility model additionally provides a kind of illumination test group, the aircraft comprising some above-mentioned illuminometers based on flight location and the long-range master control device of dividing level signal to be connected with the controller of each described aircraft.
Further improvement: the control zone that described long-range master control device comprises the bearing data for inputting surveyed area and the transceiver be connected with described control zone signal, transmitting and receiving module is provided with in the controller of each described aircraft, described transceiver is connected with transmitting and receiving module signal, bearing data is sent to transmitting and receiving module by described transceiver, and brightness value is sent to transceiver by described transmitting and receiving module.
Further improvement: described long-range master control device also comprises viewing area, described viewing area is connected with control zone, transceiver and receives display orientation data and brightness value.
Illuminometer based on flight location of the present utility model by arranging illuminometer and displacement location device on board the aircraft, and is controlled by controller, thus can save more people's Force meansurement, saves time and cost, and accurate positioning, improve measuring accuracy.And form graticule mesh shape measuring point can expand test area by this illumination test group, realizing multiposition tests jointly, contributes to improving the test duration and contributing to cost-saving.
Accompanying drawing explanation
Fig. 1 is the structural representation of the illuminometer based on flight location shown in the utility model one embodiment.
Fig. 2 is the using state figure of the illumination test group shown in the utility model one embodiment.
Embodiment
Below in conjunction with drawings and Examples, embodiment of the present utility model is described in further detail.Following examples for illustration of the utility model, but are not used for limiting scope of the present utility model.
Refer to Fig. 1, a kind of illuminometer based on flight location shown in the utility model one embodiment comprises aircraft 1 and remote control 2.Described aircraft 1 comprises flying body 11, be arranged on illuminometer 12 on described flying body 11 and displacement location device (not shown) and controller 13, the screw propeller 15 that described flying body 11 has housing 14 and is arranged on housing 14, this flying body 11 can level, vertically movement, can also rotate freely.In the present embodiment, this housing 14 is rectangular structure, and described screw propeller 15 is arranged on the top of housing 14, and described illuminometer 12 is arranged on the bottom of described housing 14.Described controller 13 is connected with flying body 11 and displacement location device respectively, described displacement location device can utilize GPS method, or use other locator meamss existing, as ZigBee technology etc., realize the detection and positioning in orientation, when specifically locating, it can according to the morphological relationship with tested reference field, tester the disposable posture is to form vertical relation with test benchmark face, and convertible different distance is tested.The position of monitored flying body 11 is also sent to controller 13 by the position of described displacement location device Real-Time Monitoring flying body 11, and the position of the flying body 11 that described controller 13 monitors according to displacement location device controls the moving direction of flying body 11 and/or amount of movement and/or sense of rotation.Described illuminometer 12 is connected with controller 13 and controls it by controller 13 and starts to detect brightness value, and detected brightness value is sent to controller 13 by described illuminometer 12.Transmitting and receiving module (not shown) is provided with in described controller 13.Described remote control 132 is connected with controller 13 signal, and control described controller 13, in the present embodiment, described remote control 2 is two, be respectively mobile client 21 (as IPAD, mobile phone) and fixed clients 22, wherein, each described remote control 2 comprises the control zone 23 of the bearing data for inputting surveyed area, the transceiver (not shown) be connected with described control zone 23 signal and viewing area 24.Described transceiver is connected with transmitting and receiving module signal, and to carry out exchanges data, bearing data is sent to transmitting and receiving module by described transceiver, and described transmitting and receiving module receives this bearing data and brightness value is sent to transceiver.There is in this control zone 23 button (non-label) inputting bearing data.Described viewing area 24 is connected with control zone 23, transceiver, and receives display orientation data and brightness value.
The above-mentioned illuminometer 12 based on flight location works as follows: first user is by the button on the control zone 23 of pressing remote control 132, the bearing data of the required surveyed area of input, then, this bearing data shows by viewing area 24, be sent to transmitting and receiving module by this bearing data of transceiver simultaneously, after transmitting and receiving module receives this bearing data, this bearing data be delivered to controller 13; After controller 13 receives described bearing data, compare with the position of the flying body 11 by displacement location device Real-Time Monitoring simultaneously, then control flying body 11 moving direction and/or amount of movement and/or sense of rotation to reach the position of specifying; After reaching assigned address, described controller 13 drives illuminometer 12 to start, illuminometer 12 detects brightness value and brightness value is sent to controller 13, this controller 13 is sent to transceiver by the transmitting and receiving module of its inside again, then passes to viewing area 24 to show this brightness value by transceiver.
In other embodiments, remote control 132 should can not be set based on the illuminometer 12 of flight location.Before detection, the bearing data of required surveyed area first can be inputted in controller 13, after starting this illuminometer 12 of locating based on flight, by controller 13 according to this bearing data and in combination with the position of displacement location device Real-Time Monitoring flying body 11, to compare, control flying body 11 moving direction and/or amount of movement and/or sense of rotation to reach the position of specifying, after reaching assigned address, described controller 13 drives illuminometer 12 to start again, illuminometer 12 detects brightness value and will be sent to controller 13, and this brightness value is shown on flying body 11, or, after detection completes, controller 13 controls flying body 11 and returns, then brightness value and bearing data is read by data fetch device.When directly showing on flying body 11, this flying body 11 is provided with the display circuit be connected with described controller 13 signal to show brightness value and bearing data, in addition, in controller 13, the mode of the bearing data of the required surveyed area of input can for input to controller 13 by external unit; Or enter key is set on controller 13, then manually inputs the bearing data of required surveyed area; The gps data clicked input automatically and follow the tracks of is set on the controller.
In the present embodiment, described aircraft 1 is also provided with to the power supply (not shown) of illuminometer 12, displacement location device and controller 13 power supply.
The above-mentioned illuminometer 12 based on flight location by arranging illuminometer 12 and displacement location device on aircraft 1, and controlled by controller 13, thus more people's Force meansurement can be saved, save time and cost, and accurate positioning, improve measuring accuracy.
Refer to Fig. 2, the aircraft 1 that a kind of illumination test group of the present utility model comprises some above-mentioned illuminometers 12 based on flight location and the long-range master control device (not shown) be connected with controller 13 points of level signals of each described aircraft 1.The control zone that described long-range master control device comprises the bearing data for inputting surveyed area and the transceiver be connected with described control zone signal, transmitting and receiving module is provided with in the controller of each described aircraft 1, described transceiver is connected with transmitting and receiving module signal, bearing data is sent to transmitting and receiving module by described transceiver, and brightness value is sent to transceiver by described transmitting and receiving module.Described long-range master control device also comprises viewing area, and described viewing area is connected with control zone, transceiver and receives display orientation data and brightness value.When reality uses, each aircraft 1 can require to carry out detection position control according to level reference or vertical reference face.
When this illumination test group uses, long-range master control device inputs respectively some bearing datas needing surveyed area, then, these bearing datas show by viewing area, by transceiver, these bearing datas are sent respectively the transmitting and receiving module of each aircraft 1, this bearing data is delivered to its controller 13 after receiving corresponding bearing data by each transmitting and receiving module simultaneously, then after the controller 13 of each aircraft 1 receives described bearing data, compare with the position of the flying body 11 by displacement location device Real-Time Monitoring simultaneously, then flying body 11 moving direction and/or amount of movement and/or sense of rotation is controlled to reach the position of specifying, when illumination test group uses, surveyed area involved by general group can participate in containing multiple aircraft 1, now, multiple aircraft 1 needs to arrange according to certain rules, the detection ordering comprising the phase mutual edge distance between the orientation of aircraft 1 and aircraft 1 and cause thus, such arrangement needs design in advance, make the concrete bearing data of each aircraft 1 variant.Fig. 2 is the test signal of horizontal illumination value and vertical illumination value, and in the first surveyed area 201, about three aircraft of arranging 1, at test vertical illuminance, can record the vertical illumination value in three differing heights regions; In the second surveyed area 202, there is the aircraft 1 of six horizontal arrangement at test water planar illumination, the horizontal illumination value that six highly identical, region is different can be recorded; In the 3rd surveyed area 203, about three aircraft of arranging 1, at test water planar illumination, can record the horizontal illumination value of three differing heights; After multiple aircraft 1 reaches assigned address, described controller 13 drives illuminometer 12 to start, illuminometer 12 detects brightness value and brightness value is sent to controller 13, this controller 13 is sent to transceiver by the transmitting and receiving module of its inside again, then passes to viewing area 24 to show the brightness value corresponding to each bearing data by transceiver.Form graticule mesh shape measuring point by this illumination test group and can expand test area, meet the common test request that multiposition is interior at one time, shorten the integrated testability time and contribute to cost-saving.Certainly, also can according to the real time demand at scene, setting order point Different periods ground is tested successively.
It is emphasized that: be only preferred embodiment of the present utility model above, not any pro forma restriction is done to the utility model, every above embodiment is done according to technical spirit of the present utility model any simple modification, equivalent variations and modification, all still belong in the scope of technical solutions of the utility model.
Claims (10)
1. the illuminometer based on flight location, it is characterized in that: comprise aircraft, described aircraft comprises flying body, be arranged on illuminometer on described flying body and displacement location device and controller, described controller is connected with flying body and displacement location device respectively, the position of monitored flying body is also sent to controller by the position of described displacement location device Real-Time Monitoring flying body, the position of the flying body that described controller monitors according to displacement location device controls the moving direction of flying body and/or amount of movement and/or sense of rotation, described illuminometer is connected with described controller and controls it by described controller and starts to detect brightness value, and detected brightness value is sent to controller by described illuminometer.
2. as claimed in claim 1 based on the illuminometer of flight location, it is characterized in that: described flying body is provided with the display circuit be connected with described controller signals to show brightness value and bearing data.
3. the illuminometer based on flight location according to claim 2, is characterized in that: described controller be provided with the enter key/of the bearing data manually inputting required surveyed area or click the gps data automatically inputting and follow the tracks of.
4. as the illuminometer based on flight location in claims 1 to 3 item as described in any one, it is characterized in that: the described illuminometer based on flight location also comprises remote control, described remote control is connected with controller signals, and controls described controller.
5. as claimed in claim 4 based on the illuminometer of flight location, it is characterized in that: the control zone that described remote control comprises the bearing data for inputting surveyed area and the transceiver be connected with described control zone signal, transmitting and receiving module is provided with in described controller, described transceiver is connected with transmitting and receiving module signal, bearing data is sent to transmitting and receiving module by described transceiver, and illumination is sent to transceiver by described transmitting and receiving module.
6., as claimed in claim 5 based on the illuminometer of flight location, it is characterized in that: described remote control also comprises viewing area, described viewing area is connected with control zone, transceiver and receives display orientation data and brightness value.
7., as claimed in claim 1 based on the illuminometer of flight location, it is characterized in that: described aircraft is provided with the power supply of powering to illuminometer, displacement location device and controller.
8. an illumination test group, is characterized in that: comprise some aircraft as the illuminometer based on flight location in claims 1 to 3 item as described in any one and with each as described in the controller of the aircraft long-range master control device of dividing level signal to be connected.
9. illumination test group as claimed in claim 8, it is characterized in that: the control zone that described long-range master control device comprises the bearing data for inputting surveyed area and the transceiver be connected with described control zone signal, transmitting and receiving module is provided with in the controller of each described aircraft, described transceiver is connected with transmitting and receiving module signal, bearing data is sent to transmitting and receiving module by described transceiver, and brightness value is sent to transceiver by described transmitting and receiving module.
10. illumination test group as claimed in claim 9, it is characterized in that: described long-range master control device also comprises viewing area, described viewing area is connected with control zone, transceiver and receives display orientation data and brightness value.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520196438.1U CN204575195U (en) | 2015-04-01 | 2015-04-01 | Based on illuminometer and the illumination test group of flight location |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520196438.1U CN204575195U (en) | 2015-04-01 | 2015-04-01 | Based on illuminometer and the illumination test group of flight location |
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| CN204575195U true CN204575195U (en) | 2015-08-19 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104713639A (en) * | 2015-04-01 | 2015-06-17 | 苏州大学 | Illumination tester based on aeroplane positioning and illumination testing group |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104713639A (en) * | 2015-04-01 | 2015-06-17 | 苏州大学 | Illumination tester based on aeroplane positioning and illumination testing group |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150819 Termination date: 20180401 |
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| CF01 | Termination of patent right due to non-payment of annual fee |