CN205311921U - Take photo by plane with burnt control system and aircraft - Google Patents
Take photo by plane with burnt control system and aircraft Download PDFInfo
- Publication number
- CN205311921U CN205311921U CN201520951955.5U CN201520951955U CN205311921U CN 205311921 U CN205311921 U CN 205311921U CN 201520951955 U CN201520951955 U CN 201520951955U CN 205311921 U CN205311921 U CN 205311921U
- Authority
- CN
- China
- Prior art keywords
- burnt
- aircraft
- telepilot
- plane
- communication unit
- 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
- 238000004891 communication Methods 0.000 claims abstract description 124
- 238000005516 engineering process Methods 0.000 claims description 22
- 238000000034 method Methods 0.000 claims description 9
- 238000010295 mobile communication Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 6
- 230000000694 effects Effects 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000000060 site-specific infrared dichroism spectroscopy Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000001052 transient effect Effects 0.000 description 1
Abstract
The utility model provides a take photo by plane with burnt control system, including be used for producing with burnt control command with burnt remote controller (3), and the camera lens pivoted that is used for setting up shooting device (23) on aircraft (1) according to the drive with burnt control command is with burnt ware motor (24), with with burnt remote controller (3) communication connection in order to receive aircraft remote controller (4) with burnt control command, be used for with aircraft remote controller (4) communication connection in order to receive aircraft communication unit (18) with burnt control command, and be used for according to driving the camera lens pivoted control system who shoots device (23) with burnt ware motor (24) with the control of burnt control command. The utility model provides an aircraft (1). The utility model discloses a take photo by plane with burnt control system and aircraft can realize control camera lens focus or light ring in the field of taking photo by plane with following burnt control command by means of being conveyed to the aircraft by the aircraft remote controller, can show to promote the effect of taking photo by plane.
Description
Technical field
The utility model relates to one and takes photo by plane with burnt Controlling System, particularly relates to a kind of based on following burnt Controlling System without man-machine taking photo by plane and use the aircraft of the method.
Background technology
Existing generally comprise hand-held remote control end and motor receiving end with burnt system, after hand-held remote control end gets handle position of rotation, instruction is sent to motor receiving end by wireless radio frequency modules, motor receiving end controls electric machine rotation again after receiving instruction, thus drive camera lens to rotate, it is achieved the change of lens focus or aperture. Existing with burnt system be separate without man-machine remote control and receiving system.
But taking photo by plane in application, the existing remote control distance with burnt system has been exceeded without man-machine flying distance, and along with apart from becoming far away, can make greatly increase with the burnt hand-held remote control end of system and the communication time delay of motor receiving end and card occurs, which results in and directly cannot be applied in existing without man-machine field of taking photo by plane with burnt system.
Practical novel content
In view of this, it is necessary to provide one to take photo by plane with burnt Controlling System and aircraft, it is possible to effectively control lens focus and aperture.
One is taken photo by plane with burnt Controlling System, comprise for generation of with burnt steering order with burnt telecontrol device, and follow burnt device motor for what rotate according to the described camera lens following burnt steering order driving to arrange filming apparatus on board the aircraft, described taking photo by plane also comprises with Jiao's Controlling System: aircraft telepilot, and described aircraft telepilot and described communication connection with Jiao's telecontrol device follow burnt steering order to receive described following described in burnt telecontrol device transmission; It dead end communication unit, for communicating to connect to receive from following burnt steering order described in described aircraft telepilot with described aircraft telepilot;And Controlling System, follow burnt device motor to drive the camera lens of described filming apparatus to rotate for what receive according to described sky dead end communication unit with burnt steering order control is described.
Further, described sky dead end communication unit is rf receiver and transmitter.
Further, described rf receiver and transmitter is that its running frequency is at the microwave range of 5.728GHz 5.85GHz for performing the application specific integrated circuit receiving and dispatching microwave signal.
Further, described sky dead end communication unit and described filming apparatus directly communicate to connect, for the image that described filming apparatus is taken is sent to described aircraft telepilot.
Further, described in take photo by plane and also comprise terminal display screen with burnt Controlling System, described terminal display screen is used for the graphic information of display in real time captured by described filming apparatus.
Further, described terminal display screen is the display screen arranged on the terminating unit independent of described aircraft telepilot, described terminating unit and the communication connection of the described aircraft telepilot graphic information to be taken by filming apparatus described in described aircraft remote control.
Further, described terminal display screen and described aircraft telepilot are wholely set.
Further, described terminal display screen and described be wholely set with burnt telepilot, described obtains described graphic information to show described graphic information in described terminal display screen with burnt telepilot from described aircraft telepilot.
Further, described Controlling System is flying vehicles control system, and described flying vehicles control system communicates unit from following burnt control command described in described aircraft remote control by described sky dead end.
Further, this flying vehicles control system and described filming apparatus communicate to connect to receive described graphic information, and by described sky dead end communication unit, described graphic information is sent to described aircraft telepilot.
Further, described Controlling System is cloud platform control system, and described cloud platform control system is also described with burnt steering order to receive with the communication connection of described flying vehicles control system.
Further, described cloud platform control system and the communication connection of described flying vehicles control system are to transmit described graphic information to described flying vehicles control system, and described graphic information is sent to described aircraft telepilot by described flying vehicles control system again.
Further, described Controlling System is cloud platform control system, described cloud platform control system and the communication connection of described filming apparatus are for obtaining the graphic information of described filming apparatus shooting, and by described sky dead end communication unit, described graphic information is sent to described aircraft telepilot.
Further, described filming apparatus is provided with filming apparatus communication unit, described filming apparatus communication unit and the communication connection of described aircraft telepilot, for directly transmitting described graphic information to described aircraft telepilot.
Further, described aircraft telepilot also comprises input unit, and described input unit is used for producing flight controlling instruction to control the flight of described aircraft according to user operation.
Further, described communicated to connect by wherein one or more modes in wired, bluetooth, infrared, WIFI, mobile communication network with burnt telepilot and described aircraft telepilot.
Further, described graphic information adopts encryption technology to be encrypted when transmitting.
Further, described aircraft telepilot is provided with holding part, described can removably be accommodated in described holding part with burnt telecontrol device.
Further, the inwall of described holding part is provided with electrical connection section, described be provided with the connectivity port corresponding with described electrical connection section with burnt telecontrol device, when described be accommodated in described holding part with burnt telecontrol device time, described connectivity port is electrically connected with described electrical connection section.
Further, described when departing from described holding part with burnt telecontrol device, it is connected with described aircraft telepilot cableless communication.
A kind of aircraft, the cloud platform comprising fuselage and be connected with described fuselage, described cloud platform is for loading filming apparatus and follows burnt device motor, it is described that with burnt device motor, for driving, the camera lens of described filming apparatus rotates, described aircraft also comprises: sky dead end communication unit, and dead end communication unit in described sky is used for from an aircraft remote control with burnt steering order; And Controlling System, described Controlling System is used for driving the camera lens of described filming apparatus to rotate with burnt steering order control is described with burnt device motor according to described.
Further, dead end communication unit in described sky is sky dead end communication unit, and dead end communication unit in described sky is rf receiver and transmitter.
Further, dead end communication unit in described sky is also for receiving the flight controlling instruction from described aircraft telepilot, and described Controlling System is also for the flight of aircraft according to described flight controlling instruction control.
Further, described Controlling System also for obtaining the graphic information of described filming apparatus shooting from described filming apparatus, and dead end communication unit in described sky also for being sent to described aircraft telepilot by described graphic information.
Further, described cloud platform comprises cloud platform control system, and for controlling, described cloud platform rotates around multiaxis described cloud platform control system relative to the fuselage of described aircraft.
Further, described Controlling System is cloud platform control system, and described cloud platform control system is connected to receive described with burnt telecommand with described sky dead end communication unit communication.
Further, described sky dead end communication unit is arranged on described cloud platform control system.
Further, described sky dead end communication unit is arranged on described filming apparatus.
Further, graphic information captured by described filming apparatus is directly sent to described aircraft telepilot by the described sky dead end unit that communicates.
Further, described aircraft also comprises sensor, the flight data in aircraft flight process described in described sensor sense, and described flight data are also sent to described aircraft telepilot by described sky dead end communication unit by described Controlling System.
Described taking photo by plane follows burnt system and aircraft, can be sent to aircraft with burnt steering order by aircraft telepilot, it is achieved that control lens focus or aperture in field of taking photo by plane, can significantly promote aerial photography effect.
Accompanying drawing explanation
Fig. 1 be the utility model implement mode provide a kind of without man-machine structural representation.
Fig. 2 be the utility model implement mode provide a kind of without man-machine module diagram.
Fig. 3 is a kind of structural representation with burnt system of taking photo by plane that the utility model enforcement mode provides.
Fig. 4 is a kind of stereographic map with burnt Controlling System of taking photo by plane that the utility model enforcement mode provides.
Fig. 5 is the module diagram taken photo by plane shown in Fig. 3 with burnt Controlling System.
Fig. 6 is the structural representation that figure the utility model implements a kind of aircraft telepilot that mode provides.
A kind of schema with Jiao method of taking photo by plane that Fig. 7 provides for the utility model enforcement mode.
A kind of schema with Jiao method of taking photo by plane that Fig. 8 provides for another enforcement mode of the utility model.
Main element nomenclature
| Aircraft | 1 |
| Fuselage | 10 |
| Flying vehicles control system | 12 |
| Storing device | 14 |
| Sensor | 16 |
| First communication unit | 18 |
| Cloud platform | 2 |
| Cloud platform control system | 20 |
| Connection mechanism | 21 |
| Support mechanism | 22 |
| Filming apparatus | 23 |
| With burnt device motor | 24 |
| With burnt telepilot | 3 |
| Knob structure | 30 |
| Angle sensor device | 32 |
| Controller | 33,44 |
| 2nd communication unit | 34 |
| Aircraft telepilot | 4 |
| Third communication unit | 40 |
| Input unit | 42 |
| 4th communication unit | 46 |
| 5th communication unit | 48 |
| Terminal display screen | 5 |
| Aircraft | 1 |
| Fuselage | 10 |
| Flying vehicles control system | 12 |
| Storing device | 14 |
| Sensor | 16 |
| First communication unit | 18 |
| Cloud platform | 2 |
| Cloud platform control system | 20 |
| Connection mechanism | 21 |
| Support mechanism | 22 |
| Filming apparatus | 23 |
| With burnt device motor | 24 |
| With burnt telepilot | 3 |
| Knob structure | 30 |
| Angle sensor device | 32 |
| Controller | 33,44 |
| 2nd communication unit | 34 |
| Aircraft telepilot | 4 |
| Third communication unit | 40 |
| Input unit | 42 |
| 4th communication unit | 46 |
| 5th communication unit | 48 |
| Terminal display screen | 5 |
Following embodiment will illustrate the utility model further in conjunction with above-mentioned accompanying drawing.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that 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 other embodiments all obtained under creative work prerequisite, all belong to the scope of the utility model protection.
It should be noted that, when assembly is called as " being fixed on " another assembly, it can directly on another assembly or can also there is assembly placed in the middle. When an assembly is considered as " connection " another assembly, it can be directly connected to another assembly or may there is assembly placed in the middle simultaneously. When an assembly is considered as " being arranged at " another assembly, it can be set directly on another assembly or may there is assembly placed in the middle simultaneously. Term as used herein " vertical ", " level ", "left", "right" and similar statement are just for illustrative purposes.
Unless otherwise defined, all technology used herein and scientific terminology are identical with belonging to the implication that those skilled in the art of the present utility model understand usually. The term used in specification sheets of the present utility model herein is the object in order to describe specific embodiment, is not intended to be restriction the utility model. Term as used herein " and/or " comprise arbitrary and all combinations of one or more relevant Listed Items.
Referring to shown in Fig. 1 and Fig. 2, the utility model implements mode provides a kind of aircraft 1, and described aircraft 1 can be the aircraft that rotor aircraft, Fixed Wing AirVehicle or the fixing wing mix with rotor. Wherein said rotor can be single rotor, DCB Specimen, three rotors, four rotors, six rotors and eight rotors etc. In the present embodiment, described aircraft 1 is rotor unmanned flight's device (UnmannedAerialVehicle, UAV).
Described aircraft 1 comprises fuselage 10, flying vehicles control system 12, storing device 14, sensor 16, first communication unit 18 and cloud platform 2. In present embodiment, described flying vehicles control system 12, storing device 14, sensor 16 and the first communication unit 18 are all arranged on described fuselage 10 with cloud platform 2. It should be appreciated that in other implementations, other positions that described sensor 16, described first communication unit 18 can be arranged on described aircraft 1 except described fuselage 10, such as, on the machine arm (figure does not indicate) of aircraft 1.
Described flying vehicles control system 12, for controlling the flight of described aircraft 1, includes but not limited to, the flight velocity of control aircraft 1, highly, attitude etc. In one embodiment, quantity and the type of described sensor 16 can be multiple, include but not limited to, Inertial Measurement Unit, baroceptor, temperature sensor, acceleration transducer, position transducer etc. Described sensor 16 and filming apparatus 23 are communicated to connect by wired or wireless mode and described flying vehicles control system 12, described flying vehicles control system 12 can obtain the various flight data of described aircraft 1 from described sensor 16, include but not limited to, highly, acceleration (pitching, rolling, and driftage), posture, geographical position, speed, external air temperature, and/or air pressure etc.Described flying vehicles control system 12 can obtain the image etc. of described filming apparatus 23 shooting from filming apparatus 23. The various flight data obtained can be saved in the storing device 14 of described aircraft 1.
Described first communication unit 18 for an aircraft telepilot 4(Fig. 3) communication connection, for receiving the flight instruction from aircraft telepilot 4. The flight of flight instruction control aircraft that described flying vehicles control system 12 receives according to described first communication unit 18, comprise take off with land, accelerate, slow down, particular course flight, given pose flight etc. Described first communication unit 18 adopts communication, such as, can be a kind of rf receiver and transmitter. In the present embodiment, described first communication unit 18 also for receive from described aircraft telepilot 4 with burnt control command, described rotate for controlling the camera lens of described filming apparatus 23 with burnt control command. Described flying vehicles control system 12 is also for being sent to described cloud platform 2 by described with burnt control command.
Described first communication unit 18 can be a rf receiver and transmitter, and illustratively, described rf receiver and transmitter can be made up of several elements, comprises radio frequency (RadioFrequency, RF) strainer, and described RF strainer only allows specification signal wave band to pass through. Described rf receiver and transmitter also can comprise a RF front end, and described RF front end is a unicircuit, for performing: described in down converted, RF signal is to intermediate frequency (IntermediateFrequency, IF) signal; Amplify described IF signal, adopt IF strainer to filter described signal and adopt the analog to digital converter in chip to change described signal to two numerical digit component: mark and magnitude. One phase-locked loop filter be used to using described down converted device with as time base reference crystal together be built into described RF front end. The gain of the IF amplifier of described RF front end controls by automatic growth control (Automaticgaincontrol, AGC) signal.
In the described embodiment, described rf receiver and transmitter can be one for performing the application specific integrated circuit receiving and dispatching microwave signal, and its running frequency can at the microwave range of 5.728GHz 5.85GHz. Described rf receiver and transmitter receives by antenna and transmission tick.
Described cloud platform 2 comprises cloud platform control system 20, connection mechanism 21 and supports mechanism 22. Described cloud platform control system 20 rotates around multiaxis relative to the fuselage 10 of described aircraft 1 for controlling described cloud platform 2. Described cloud platform control system 20 also for communicate to connect with described flying vehicles control system 12 to receive from described flying vehicles control system 12 with burnt control command. Described cloud platform control system 20 communicates to connect by wireless or wired mode and described flying vehicles control system 12, wired mode comprises various port and connects, such as general serial bus (universalserialbus, USB), controller local area network (Controllerareanetwork, CAN), serial and/or other standards network connect, (Inter-IntegratedCircuit, I2C) bus etc. between unicircuit; Wireless mode comprises bluetooth, infrared rays, Wireless Fidelity (WirelessFidelity, WiFi) etc.
Described support mechanism 22 is arranged on fuselage 10 by connection mechanism 21, and for carrying filming apparatus 23 and follow burnt device motor 24. Described connection mechanism 21 can be multi-spindle rotary mechanism so that described support mechanism 22 can rotate around multiaxis and convert shooting direction and/or the angle of described filming apparatus 23.Described be connected with the camera lens of described filming apparatus 23 with burnt device motor 24, for driving the camera lens rotation of described filming apparatus 23 under the control of cloud platform control system 20 thus change lens focus or the aperture effect of described filming apparatus 23. In the present embodiment, described Jiao's of following device motor 24 passes through gear (not shown) and is connected with the camera lens of described filming apparatus 23, described rotate under the control of cloud platform control system 20 with burnt device motor 24, the camera lens of power to described filming apparatus 23 is transmitted, so that the camera lens of described filming apparatus 23 rotates by gear. In other embodiments, described Jiao's of following device motor 24 can also be connected with the camera lens of described filming apparatus 23 by mode of connection that other are suitable for, as long as the camera lens that can drive described filming apparatus 23 can rotate under the power wheel drive with burnt device motor 24, such as, belt connection etc. In the present embodiment, described arrange independent of described filming apparatus 23 with burnt device motor 24, in other embodiments, described can be wholely set with described filming apparatus 23 with burnt device motor 24.
Referring to shown in Fig. 3, a kind of the taking photo by plane that implementing mode for the utility model provides follows the schematic diagram of burnt system. Described taking photo by plane follows burnt system to comprise flying vehicles control system 12, cloud platform control system 20, filming apparatus 23, with burnt device motor 24, follow Jiao's telepilot 3, aircraft telepilot 4 and terminal display screen 5.
Described Jiao's of following telepilot 3 is for following burnt control command according to user operation generation, and described Jiao's of following control command follows Jiao's telepilot 3 to be sent to described aircraft telepilot 4 from described in a wired or wireless manner; Described aircraft telepilot 4 is sent to described flying vehicles control system 12 with burnt control command by communications such as twireless radio-frequency communications by described again, and described flying vehicles control system 12 is resent to described cloud platform control system 20 by described with burnt control command. Described producing motivating force with burnt device motor 24 under the control of described cloud platform control system 20, the camera lens ordering about described filming apparatus 23 rotates lens focus and/or the aperture effect to change described filming apparatus 23.
In an embodiment illustrated, described aircraft telepilot 4 can be provided with holding part, described can removably be accommodated in described holding part with burnt telecontrol device 3. The inwall of described holding part is provided with electrical connection section, described is provided with the connectivity port corresponding with described electrical connection section with burnt telecontrol device 3, when described be accommodated in described holding part with burnt telecontrol device 3 time, described connectivity port is electrically connected with described electrical connection section. Described when departing from described holding part with burnt telecontrol device 3, it is connected with described aircraft telepilot cableless communication.
Described terminal display screen 5 can be the indicating meter of a computer equipment, or the display screen of the handheld device such as mobile phone, panel computer. In other embodiments, the part that described terminal display screen 5 also can be integrated on described aircraft telepilot 4 as described aircraft telepilot 4. In another alternative embodiments, described terminal display screen 5 can also be integrated in described with becoming a described part with burnt telepilot 3 on burnt telepilot 3. In an alternative embodiments again, described all connect with burnt telepilot 3 and described aircraft telepilot 4 or it is provided with display screen, being respectively used to show the image of described filming apparatus 23 shooting and the described aircraft 1 flight data in flight course. Described terminal display screen 5 can be used for showing in real time the flight data of described aircraft 1 in flight course and/or the image captured in the flight course of described aircraft 1 of described filming apparatus 23.
Referring to shown in Fig. 4 and Fig. 5, the one that implementing mode for the utility model provides follows burnt telepilot 3. Described comprise knob structure 30, angle sensor device 32, controller 33 and the 2nd communication unit 34 with burnt telepilot 3. Described knob structure 30 can be operated to rotate relative to the described body with burnt telepilot 3. The rotation angle information of described knob structure 30 surveyed by described angle sensor device 32 for feeling. The rotation angle information that described controller 33 is surveyed for feeling according to described angle sensor device 32 produces with burnt control command.
Described 2nd communication unit 34 is for communicating to connect to be sent to described aircraft telepilot 4 by described with burnt control command with described aircraft telepilot 4. Described 2nd communication unit 34 can adopt wired or wireless mode. Described wired mode is comprised and being connected by communication port, such as USB interface etc. Described wireless mode can adopt the radio communication system of any classification, such as, and bluetooth, infrared rays, Wireless Fidelity (WirelessFidelity, WiFi), honeycomb technology, satellite, and broadcast. Wherein said honeycomb technology can comprise the mobile communication technology such as the s-generation (2G), the third generation (3G), forth generation (4G) or the 5th generation (5G). Described 3G and 4G technology is based on the mobile communication standard meeting the international standard that described Union Internationale des Telecommunications (InternationalTelecommunicationsUnion, ITU) is promulgated. Described 3G and 4G technology can provide every second 200 kilobit to the information transfer rate of every second a few gigabit bit, so that it is widely used in adopting large bandwidth transmission high-resolution image and video. 3G technology typically refers to those and meets international mobile communication 2000(InternationalMobileTelecommunications2000, IMT-2000) reliability of standard and the technology of transfer speed. Common business 3G technology comprises, based on system and the radio interface of spread-spectrum radio transmission technology, such as, by third generation affiliate plan (3rdGenerationPartnershipProject, 3GPP) UMTS system of stdn, W-CDMA radio interface, the TD-SCDMA radio interface that China is proposed, HSPA+UMTS issues, CDMA2000 system, and EV-DO. In addition, other technologies, such as EDGE, DECT and mobile WiMAX also meet IMT-2000, are thus also ratified as 3G standard by ITU. Correspondingly, " 3G " this word used herein comprises, but is not limited to, any technology meeting IMT-2000, comprises those technology arrived mentioned herein.
In contrast, 4G technology is construed broadly as those and meets IMT-Advanced (InternationalMobileTelecommunicationsAdvanced, IMT-Advanced) technology of specification, it requires top speed 100 megabits that reach every second when high mobility communicates, the gigabit bit that reaches every second when low movability communicates. In October, 2010, the 4G standard of ITU approval comprises enhancing LTE and strengthens wireless metropolitan area net (WirelessMAN-Advanced). But, the 4G that some commercial operations business issues serves not in full conformity with IMT-Advanced specification, such as LTE, MobileWiMAX, and TD-LTE. Correspondingly, mentioned herein to " 4G " this word comprise, but be not limited to, these technology afterwards, such as LTE, MobileWiMAX and TD-LTE, with the technology that those meet IMT-Advanced, comprise those technology arrived mentioned herein. And 5G is the next generation mobile communication standard surmounting current 4G/IMT-Advanced standard.
As shown in Figure 6, for the utility model implements the module map of a kind of aircraft telepilot 4 that mode provides. Described aircraft telepilot 4 comprises, but is not limited to, third communication unit 40, input unit 42, controller 44, the 4th communication unit 46 and the 5th communication unit 48. Described third communication unit 40 is corresponding with described 2nd communication unit 34, communicates for the unit 34 that communicate with the described 2nd to receive and follows Jiao's control command from described with burnt telepilot 3.
Described input unit 42 is the instruction inputting device of described aircraft telepilot 4, such as remote control lever, touch-screen etc., for producing input instruction to control the flight of aircraft 1 according to user operation.
Described controller 44 is for producing flight controlling order to control the flight of aircraft 1 according to described input instruction. Described controller 44 is also for being sent to described flying vehicles control system 12 with burnt control command by the 4th communication unit 46 by what received by third communication unit 40.
Described 4th communication unit 46 is the communication unit corresponding with described first communication unit 18, and its unit 18 that communicates with described first adopts identical communication, such as twireless radio-frequency communication.
Described 5th communicates unit 48 for communicating to connect with described terminal display screen 5, to transmit described flight data and/or captured image extremely described terminal display screen 5. Described 5th communication unit 48 can adopt wireless or wire communication mode, includes but not limited to, the wired mode connected by the various communication port such as USB, CAN, I2C; And the communication such as bluetooth, infrared rays, WiFi, 2G, 3G, 4G or 5G mobile communication network as above.
As shown in Figure 7, a kind of the taking photo by plane provided for the utility model enforcement mode follows the schema of burnt control method 600. According to different demand, in this schema, the order of step can change, and some step can be omitted or merge.
Step 602, the described controller 33 with burnt telepilot 3 receives the rotation angle information of described knob structure 30 from described angle sensor device 32.
Step 604, described angle information is converted to burnt control command by the described controller 33 with burnt telepilot 3.
Step 606, the described controller 33 with burnt telepilot 3 is sent to described aircraft telepilot 4 by described with burnt control command by affiliated 2nd communication unit 34. Specifically, described controller 33 is converted to, by described, the control command being suitable for described 2nd communication unit 34 and transmitting with burnt control command, and then the control command after format conversion is transferred to the described third communication unit 40 of described aircraft telepilot 4 by described 2nd communication unit 34.
Step 608, described aircraft telepilot 4 is sent to described aircraft 1 by described with burnt control command. Specifically, described aircraft telepilot 4 converts, with burnt control command, the form that suitable described 4th communication unit 46 transmits by being received by described third communication unit 40 to, and then is transferred to the first communication unit 18 of described aircraft 1 by described 4th communication unit 46.
Step 610, described flying vehicles control system 12 is sent to described cloud platform control system 20 with burnt control command described in by being received by described third communication unit 40.
Step 612, described control command is sent to described Jiao's of following device motor 24 and follows burnt device motor 24 to rotate described in control by described cloud platform control system 20.
Step 614, described Jiao's of following device motor 24 rotarily drives described camera lens and rotates to change described lens focus or aperture effect.
As shown in Figure 8, a kind of the taking photo by plane provided for another enforcement mode of the utility model follows the schema of burnt control method 800. According to different demand, in this schema, the order of step can change, and some step can be omitted or merge.
Step 802, described cloud platform control system 20 obtains the graphic information that filming apparatus 23 is taken.
Step 804, the graphic information obtained is sent to described flying vehicles control system 12 by described cloud platform control system 20.
Step 806, described graphic information is sent to described aircraft telepilot 4 by described flying vehicles control system 12.
Step 808, described graphic information is sent to described terminal display screen 5 to show described graphic information by described aircraft telepilot 4. According to shown graphic information, it may also be useful to person's adjustable vehicle teleoperation is to adjust aircraft flight posture, position and angle etc., and adjustment follows burnt control command etc. with the angle of rotation of the knob structure 30 of burnt telepilot 3 to change.
It is appreciated that, described can also be sent to described first communication unit 18 from described aircraft telepilot 4 with burnt control command after, described cloud platform control system 20 unit 18 that directly communicate with described first communicates to connect and described follows Jiao's control command to obtain from described first communication unit 18. Described cloud platform control system 20 can be communicated to connect by the upper described wired or wireless mode unit 18 that communicates with described first.
It is appreciated that, described can also be sent to described first communication unit 18 from described aircraft telepilot 4 with burnt control command after, described be directly sent to burnt control command described is rotated with burnt control command according to described with burnt device motor by described flying vehicles control system 12 with burnt device motor 24 is described to control.
It is appreciated that, described can also be sent to described first communication unit 18 from described aircraft telepilot 4 with burnt control command after, such as, can come according to the camera lens of described filming apparatus 23 being driven with burnt control command control is described to rotate with burnt device motor by an independent Controlling System (independent of described flying vehicles control system 12, cloud platform control system 20).
It can be appreciated that the graphic information captured by described filming apparatus 23 can also directly be sent to described flying vehicles control system 12 by described filming apparatus 23, described graphic information is sent to aircraft telepilot 4 by described flying vehicles control system 12 again. In this case, described flying vehicles control system 12 directly communicates to connect to obtain the graphic information captured by described filming apparatus 23 with described filming apparatus 23 by upper described wired or wireless mode.
In other embodiments, the graphic information obtained directly can also be sent to described terminal display screen 5 by described flying vehicles control system 12. In this kind of situation, described flying vehicles control system 12 communicates to connect by communication and described terminal display screen 5, and described communication can comprise 2G, 3G, 4G or 5G mobile communication system as above and radio frequency communication.
Encryption technology can be adopted it can be appreciated that described in transport process with burnt control command and/or described flight controlling order, be beneficial to the safety transmission with burnt control command and/or described flight controlling order. suitable encryption method comprises, but it is not limited to, the secret key in Internet exchanges, internet security agreement (InternetProtocolSecurity, IPsec), Kerberos, end-to-end protocol (Point-to-PointProtocol), secure transport layers agreement (TransportLayerSecurity), hide SSID, MACID filters, STATIC IP ADDRESSING (StaticIPAddressing), 802.11 security, Wired Equivalency secrecy (WiredEquivalentPrivacy, WEP), get online without being tethered to a cable protection access (Wi-FiProtectedAccess, WPA), WPA2, temporary transient secret key integrity protocol (TemporalKeyIntegrityProtocol, TKIP), authentication protocol (ExtensibleAuthenticationProtocol) can be expanded, Lightweight Extensible authentication protocol (LightweightExtensibleAuthenticationProtocol, LEAP), the protected authentication protocol expanded (ProtectedExtensibleAuthenticationProtocol, PEAP), and other commercially available encryption skills.
It can be appreciated that described indicate respectively with burnt control command and described flight controlling order can be distinguished by described aircraft telepilot 4, so that described flying vehicles control system 12 is distinguished described with Jiao's control command and described flight controlling order.
It is appreciated that, described aircraft telepilot 4 unit 18 that can be not limited to communicate with described first communicates to connect, can also be connected with other day dead end communication unit communication, such as, in other embodiments, described cloud platform control system 20, filming apparatus 23 all can be provided with and the communication unit that described aircraft telepilot 4 communicates, described aircraft telepilot 4 can directly be connected with the communication unit communication arranged on described cloud platform control system 20 or filming apparatus 23, directly transmit described with burnt control command extremely described cloud platform control system 20 or filming apparatus 23, again by described cloud platform control system 20 or filming apparatus 23 by described be forwarded to burnt control command described with burnt motor 24.
, it is possible to make other various corresponding change and distortion according to technical conceive of the present utility model, in addition, for the person of ordinary skill of the art and all these change and all should belong to the protection domain of the utility model claim with distortion.
Claims (30)
1. take photo by plane with burnt Controlling System for one kind, comprise for generation of with burnt steering order with burnt telepilot, and for according to described drive with burnt steering order that the camera lens arranging filming apparatus on board the aircraft rotates with burnt device motor, it is characterised in that: described in take photo by plane and also comprise with burnt Controlling System:
Aircraft telepilot, described aircraft telepilot and described communication connection with Jiao's telepilot follow burnt steering order to receive described following described in burnt telepilot transmission;
It dead end communication unit, for communicating to connect to receive from following burnt steering order described in described aircraft telepilot with described aircraft telepilot; And
Controlling System, follows burnt device motor to drive the camera lens of described filming apparatus to rotate for what receive according to described sky dead end communication unit with burnt steering order control is described.
2. take photo by plane with burnt Controlling System as claimed in claim 1, it is characterised in that: dead end communication unit in described sky is rf receiver and transmitter.
3. take photo by plane with burnt Controlling System as claimed in claim 2, it is characterised in that: described rf receiver and transmitter is that its running frequency is at the microwave range of 5.728GHz 5.85GHz for performing the application specific integrated circuit receiving and dispatching microwave signal.
4. take photo by plane with burnt Controlling System as claimed in claim 1, it is characterised in that: described sky dead end communication unit and described filming apparatus directly communicate to connect, for the image that described filming apparatus is taken is sent to described aircraft telepilot.
5. take photo by plane as claimed in claim 1 with burnt Controlling System, it is characterised in that: described in take photo by plane and also comprise terminal display screen with burnt Controlling System, described terminal display screen is used for the graphic information of display in real time captured by described filming apparatus.
6. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterized in that: described terminal display screen is the display screen arranged on the terminating unit independent of described aircraft telepilot, described terminating unit and the communication connection of the described aircraft telepilot graphic information to be taken by filming apparatus described in described aircraft remote control.
7. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterised in that: described terminal display screen and described aircraft telepilot are wholely set.
8. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterized in that: described terminal display screen and described be wholely set with burnt telepilot, described obtain described graphic information to show described graphic information in described terminal display screen with burnt telepilot from described aircraft telepilot.
9. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterised in that: described Controlling System is flying vehicles control system, and described flying vehicles control system communicates unit from following burnt control command described in described aircraft remote control by described sky dead end.
10. take photo by plane with burnt Controlling System as claimed in claim 9, it is characterized in that: this flying vehicles control system and described filming apparatus communicate to connect to receive described graphic information, and described graphic information is sent to described aircraft telepilot by described sky dead end communication unit.
11. take photo by plane with burnt Controlling System as claimed in claim 9, it is characterised in that: described Controlling System is cloud platform control system, and described cloud platform control system is also described with burnt steering order to receive with the communication connection of described flying vehicles control system.
12. take photo by plane with burnt Controlling System as claimed in claim 11, it is characterized in that: described cloud platform control system and the communication connection of described flying vehicles control system are to transmit described graphic information to described flying vehicles control system, and described graphic information is sent to described aircraft telepilot by described flying vehicles control system again.
13. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterized in that: described Controlling System is cloud platform control system, described cloud platform control system and the communication connection of described filming apparatus are for obtaining the graphic information of described filming apparatus shooting, and by described sky dead end communication unit, described graphic information is sent to described aircraft telepilot.
14. take photo by plane with burnt Controlling System as claimed in claim 5, it is characterized in that: described filming apparatus is provided with filming apparatus communication unit, described filming apparatus communication unit and the communication connection of described aircraft telepilot, for directly transmitting described graphic information to described aircraft telepilot.
Taking photo by plane as described in 15. items as arbitrary in claim 1～14 follows burnt Controlling System, it is characterized in that: described aircraft telepilot also comprises input unit, described input unit is used for producing flight controlling instruction to control the flight of described aircraft according to user operation.
Taking photo by plane with burnt Controlling System as described in 16. items as arbitrary in claim 1～14, it is characterised in that: described communicated to connect by wherein one or more modes in wired, bluetooth, infrared, WIFI, mobile communication network with burnt telepilot and described aircraft telepilot.
Taking photo by plane as described in 17. items as arbitrary in claim 5～14 follows burnt Controlling System, it is characterised in that: described graphic information adopts encryption technology to be encrypted when transmitting.
Taking photo by plane with burnt Controlling System as described in 18. items as arbitrary in claim 1～14, it is characterised in that: described aircraft telepilot is provided with holding part, described can removably be accommodated in described holding part with burnt telepilot.
19. take photo by plane with burnt Controlling System as claimed in claim 18, it is characterized in that: the inwall of described holding part is provided with electrical connection section, described it is provided with the connectivity port corresponding with described electrical connection section with burnt telepilot, when described be accommodated in described holding part with burnt telepilot time, described connectivity port is electrically connected with described electrical connection section.
20. take photo by plane with burnt Controlling System as claimed in claim 19, it is characterised in that: described when departing from described holding part with burnt telepilot, it is connected with described aircraft telepilot cableless communication.
21. 1 kinds of aircraft, the cloud platform comprising fuselage and be connected with described fuselage, described cloud platform is for loading filming apparatus and follows burnt device motor, and described with burnt device motor, for driving, the camera lens of described filming apparatus rotates, it is characterised in that: described aircraft also comprises:
It dead end communication unit, dead end communication unit in described sky is used for from an aircraft remote control with burnt steering order; And
Controlling System, described Controlling System is used for driving the camera lens of described filming apparatus to rotate with burnt steering order control is described with burnt device motor according to described.
22. aircraft as claimed in claim 21, it is characterised in that: dead end communication unit in described sky is sky dead end communication unit, and dead end communication unit in described sky is rf receiver and transmitter.
23. aircraft as claimed in claim 22, it is characterized in that: dead end communication unit in described sky is also for receiving the flight controlling instruction from described aircraft telepilot, and described Controlling System is also for the flight of aircraft according to described flight controlling instruction control.
24. aircraft as claimed in claim 21, it is characterized in that: described Controlling System also for obtaining the graphic information of described filming apparatus shooting from described filming apparatus, and dead end communication unit in described sky also for being sent to described aircraft telepilot by described graphic information.
25. aircraft as claimed in claim 21, it is characterised in that: described cloud platform comprises cloud platform control system, and for controlling, described cloud platform rotates around multiaxis described cloud platform control system relative to the fuselage of described aircraft.
26. aircraft as claimed in claim 25, it is characterised in that: described Controlling System is cloud platform control system, and described cloud platform control system is connected to receive described with burnt telecommand with described sky dead end communication unit communication.
27. aircraft as claimed in claim 26, it is characterised in that: dead end communication unit in described sky is arranged on described cloud platform control system.
28. aircraft as claimed in claim 21, it is characterised in that: dead end communication unit in described sky is arranged on described filming apparatus.
29. aircraft as claimed in claim 28, it is characterised in that: the graphic information captured by described filming apparatus is directly sent to described aircraft telepilot by described sky dead end communication unit.
30. aircraft as described in the arbitrary item in claim 21～29, it is characterized in that: described aircraft also comprises sensor, flight data in aircraft flight process described in described sensor sense, described flight data are also sent to described aircraft telepilot by described sky dead end communication unit by described Controlling System.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520951955.5U CN205311921U (en) | 2015-11-25 | 2015-11-25 | Take photo by plane with burnt control system and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520951955.5U CN205311921U (en) | 2015-11-25 | 2015-11-25 | Take photo by plane with burnt control system and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205311921U true CN205311921U (en) | 2016-06-15 |
Family
ID=56188581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520951955.5U Expired - Fee Related CN205311921U (en) | 2015-11-25 | 2015-11-25 | Take photo by plane with burnt control system and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205311921U (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106165388A (en) * | 2015-11-25 | 2016-11-23 | 深圳市大疆创新科技有限公司 | Take photo by plane with burnt control system, take photo by plane with burnt control method and aircraft |
| CN106943753A (en) * | 2016-06-25 | 2017-07-14 | 王丽芸 | Automatically the Multi-axis aircraft toy and its control method recalled |
| CN107004343A (en) * | 2016-10-25 | 2017-08-01 | 深圳市大疆灵眸科技有限公司 | Computer-readable medium, focus tracking system, clouds terrace system, head, the data transfer control method and device of head |
| CN107278195A (en) * | 2016-11-04 | 2017-10-20 | 深圳市大疆创新科技有限公司 | Unmanned plane and antenna module |
| CN107624098A (en) * | 2016-08-31 | 2018-01-23 | 深圳市大疆灵眸科技有限公司 | Focus tracking fixed mount, unmanned vehicle and movable equipment |
| WO2018072067A1 (en) * | 2016-10-18 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Antenna component and unmanned aerial vehicle |
| CN108280981A (en) * | 2018-03-01 | 2018-07-13 | 四川智慧鹰航空科技有限公司 | A kind of miniature drone wireless control system |
| CN108447237A (en) * | 2018-03-01 | 2018-08-24 | 四川智慧鹰航空科技有限公司 | A kind of signal transmitting apparatus for unmanned plane remote control |
| WO2019080805A1 (en) * | 2017-10-26 | 2019-05-02 | 深圳市大疆创新科技有限公司 | Control apparatus, camera apparatus, flying object, control method and program |
| CN109819162A (en) * | 2019-01-22 | 2019-05-28 | 桂林飞宇科技股份有限公司 | A kind of shoot control system and method for camera cradle head system |
| CN110498039A (en) * | 2019-08-05 | 2019-11-26 | 北京科技大学 | A kind of intelligent monitor system based on bionic flapping-wing flying vehicle |
| WO2020125414A1 (en) * | 2018-12-19 | 2020-06-25 | 深圳市大疆创新科技有限公司 | Control apparatus, photography apparatus, photography system, moving body, control method and program |
| CN111712667A (en) * | 2019-07-16 | 2020-09-25 | 深圳市大疆创新科技有限公司 | Control method and device of shooting equipment, handheld cloud deck and storage medium |
| WO2022061522A1 (en) * | 2020-09-22 | 2022-03-31 | 深圳市大疆创新科技有限公司 | Photography control method and apparatus |
-
2015
- 2015-11-25 CN CN201520951955.5U patent/CN205311921U/en not_active Expired - Fee Related
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106165388A (en) * | 2015-11-25 | 2016-11-23 | 深圳市大疆创新科技有限公司 | Take photo by plane with burnt control system, take photo by plane with burnt control method and aircraft |
| CN106943753A (en) * | 2016-06-25 | 2017-07-14 | 王丽芸 | Automatically the Multi-axis aircraft toy and its control method recalled |
| CN107624098A (en) * | 2016-08-31 | 2018-01-23 | 深圳市大疆灵眸科技有限公司 | Focus tracking fixed mount, unmanned vehicle and movable equipment |
| WO2018072067A1 (en) * | 2016-10-18 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Antenna component and unmanned aerial vehicle |
| CN107004343A (en) * | 2016-10-25 | 2017-08-01 | 深圳市大疆灵眸科技有限公司 | Computer-readable medium, focus tracking system, clouds terrace system, head, the data transfer control method and device of head |
| WO2018076186A1 (en) * | 2016-10-25 | 2018-05-03 | 深圳市大疆灵眸科技有限公司 | Computer readable medium, follow focus system, pan-tilt system, pan tilt and pan tilt data transmission control method and device |
| CN107004343B (en) * | 2016-10-25 | 2019-09-17 | 深圳市大疆灵眸科技有限公司 | Computer-readable medium, focus tracking system, clouds terrace system, holder, holder data transfer control method and device |
| CN107278195A (en) * | 2016-11-04 | 2017-10-20 | 深圳市大疆创新科技有限公司 | Unmanned plane and antenna module |
| WO2018082000A1 (en) * | 2016-11-04 | 2018-05-11 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and antenna assembly |
| CN107278195B (en) * | 2016-11-04 | 2019-10-18 | 深圳市大疆创新科技有限公司 | Unmanned plane and antenna module |
| WO2019080805A1 (en) * | 2017-10-26 | 2019-05-02 | 深圳市大疆创新科技有限公司 | Control apparatus, camera apparatus, flying object, control method and program |
| CN110382359A (en) * | 2017-10-26 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Control device, photographic device, flying body, control method and program |
| US11066182B2 (en) | 2017-10-26 | 2021-07-20 | SZ DJI Technology Co., Ltd. | Control apparatus, camera apparatus, flying object, control method and program |
| CN108447237A (en) * | 2018-03-01 | 2018-08-24 | 四川智慧鹰航空科技有限公司 | A kind of signal transmitting apparatus for unmanned plane remote control |
| CN108280981A (en) * | 2018-03-01 | 2018-07-13 | 四川智慧鹰航空科技有限公司 | A kind of miniature drone wireless control system |
| WO2020125414A1 (en) * | 2018-12-19 | 2020-06-25 | 深圳市大疆创新科技有限公司 | Control apparatus, photography apparatus, photography system, moving body, control method and program |
| CN109819162A (en) * | 2019-01-22 | 2019-05-28 | 桂林飞宇科技股份有限公司 | A kind of shoot control system and method for camera cradle head system |
| CN111712667A (en) * | 2019-07-16 | 2020-09-25 | 深圳市大疆创新科技有限公司 | Control method and device of shooting equipment, handheld cloud deck and storage medium |
| CN110498039A (en) * | 2019-08-05 | 2019-11-26 | 北京科技大学 | A kind of intelligent monitor system based on bionic flapping-wing flying vehicle |
| WO2022061522A1 (en) * | 2020-09-22 | 2022-03-31 | 深圳市大疆创新科技有限公司 | Photography control method and apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205311921U (en) | Take photo by plane with burnt control system and aircraft | |
| CN106165388B (en) | It takes photo by plane with burnt control system, take photo by plane with burnt control method and aircraft | |
| EP3570132B1 (en) | System and method for data recording and analysis | |
| CN105745587B (en) | The virtual tours system and method realized using unmanned vehicle | |
| CN104750114A (en) | Portable unmanned aerial vehicle control box | |
| CN206894900U (en) | A kind of base station interference source positioning system | |
| CN204498252U (en) | A kind of police airborne video Reconnaissance system | |
| CN105352494B (en) | Cruise positioning device, cruise positioning system and method | |
| CN102519600A (en) | Flight thermal imager system and communication method thereof | |
| US20210294327A1 (en) | System and method for movable object control | |
| CN206485252U (en) | A kind of fire communication command car of use unmanned plane wireless video transmission system | |
| CN103816670A (en) | Model airplane video monitoring implementation system | |
| CN106444555A (en) | Ground forwarding-based unmanned aerial vehicle medium-short distance remote control and remote measuring system | |
| CN106657013B (en) | Unmanned aerial vehicle system and communication connection method and device thereof | |
| CN106792753A (en) | Distributed communication covering system and method | |
| WO2018090880A1 (en) | Unmanned aerial vehicle system and communication connection method and apparatus of system | |
| CN206181032U (en) | Communication connection apparatus of unmanned aerial vehicle system and this system | |
| CN206620130U (en) | A kind of UAS | |
| CN206524902U (en) | Radio transmission apparatus for the aerial dirigible system of line walking | |
| CN110531783A (en) | A kind of monitoring unmanned system based on cloud service | |
| CN206181031U (en) | Communication connection apparatus of unmanned aerial vehicle system and this system | |
| CN106357324B (en) | Unmanned aerial vehicle system and communication connection method and device thereof | |
| CN106411394B (en) | Unmanned aerial vehicle system and communication connection method and device thereof | |
| CN206618980U (en) | Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding | |
| CN202501922U (en) | Flight thermal imager system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170629 Address after: 518057 Guangdong city of Shenzhen province Nanshan District Guangdong streets south four Road No. 18 building in the West SKYWORTH semiconductor design 12 Patentee after: SZ DJI OSMO TECHNOLOGY Co.,Ltd. Address before: 518057 Guangdong province Shenzhen city Nanshan District high tech Zone South Hing a No. 9 Hongkong, Shenzhen building 6 floor Patentee before: SZ DJI TECHNOLOGY Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160615 |