CN205239910U - Remote control flight ware that can fix a point to encircle - Google Patents
Remote control flight ware that can fix a point to encircle Download PDFInfo
- Publication number
- CN205239910U CN205239910U CN201520650031.1U CN201520650031U CN205239910U CN 205239910 U CN205239910 U CN 205239910U CN 201520650031 U CN201520650031 U CN 201520650031U CN 205239910 U CN205239910 U CN 205239910U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- aircraft
- remote control
- power set
- control equipment
- 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
Abstract
The utility model provides a remote control flight ware that can fix a point to encircle, includes aircraft and remote control equipment, the aircraft includes the fuselage, installs power device and shooting device on the fuselage, its characterized in that, be equipped with GPS locator, first receiving and dispatching antenna, memory and treater on the fuselage, it all is connected with the treater electricity to shoot device, power device, GPS locator, first receiving and dispatching antenna, memory, remote control equipment includes second receiving and dispatching antenna, controls handle and controller, the second is received and dispatched the antenna, is controlled the handle and all is connected with the controller electricity. The utility model discloses a GPS locator is set for behind the centre of a circle and radius, and wind flight is realized to the aircraft, and at the wind in -process, it can continuous collection come from the data of GPS locator and calculate the assurance around gesture and moving trajectory through the treater is accurate to fly to control the ware, the fuselage is equipped with four horns and four power device of group, makes the aircraft action more nimble, balanced, and operating performance is better.
Description
Technical field
The utility model relates to the field of taking photo by plane, more particularly, relate to a kind of adjustable point around remote control distributorDevice.
Background technology
Along with scientific and technical fast development, people are increasingly deep for the research of aircraft, all kinds of flying nowRow device is applied in increasing occasion. Aircraft, because landing environmental requirement is lower, has goodOperating characteristics, can realize and take off, hover, land among a small circle, be widely used in taking photo by plane, monitor,The numerous areas such as investigation, search and rescue, control of agricultural pest.
Although aircraft has had various functions and expansion at present, as taking photo by plane, still there is ratio in the airLarger deficiency, as do not realized fixed point around shooting in the process of taking photo by plane. During especially for outdoor sportTake photo by plane, can not carry out around shooting scenery or building.
Utility model content
The technical problems to be solved in the utility model be to provide a kind of utilize two GPS fix a point around remote controlAircraft.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is as follows:
Adjustable point around a remotely-piloted vehicle, comprise aircraft and remote control equipment, described aircraft comprisesFuselage, be arranged on power set and filming apparatus on fuselage, it is characterized in that, described fuselage is provided with GPSLocator, the first dual-mode antenna, memory and processor, described filming apparatus, power set, GPS locationDevice, the first dual-mode antenna, memory are all electrically connected with processor; Described remote control equipment comprises the second transmitting-receiving skyLine, manipulation handle and controller, described the second dual-mode antenna, manipulation handle are all electrically connected with controller.
When flight after aircraft takeoff, to the correct position of intending reference object, is provided to aircraft by remote control equipmentInstruction enters fixed point pitch of the laps pattern. First, remote control equipment sends definite by the second dual-mode antenna to aircraftAround the command signal in the center of circle, then, by manipulation handle remotely-piloted vehicle fly away from around central point to apart from aroundCenter of circle correct position, remote control equipment sends the instruction of determining around radius to aircraft by the second dual-mode antennaSignal, sets after the center of circle and radius, and aircraft starts pitch of the laps, and in pitch of the laps process, aircraft can be constantlyGather from the data of GPS locator and by accurate calculating of processor and ensure around attitude and running orbit.
Further, described power set are made up of motor and propeller, and propeller is arranged on rotatinglyOn the clutch end of motor.
Further, described fuselage is provided with four horns, and described power set are provided with four groups, described four groups of powerDevice is separately fixed at the end of four horns, makes that aircraft action is more flexible, balance, and operating characteristics is better.
Further, described remote control equipment is provided with display unit, and display unit is electrically connected with controller, aobviousShowing device receives the photographic images of filming apparatus. Aircraft starts filming apparatus in the time of flight, and will be at skyIn the image that photographs send in the display unit of remote control equipment, manipulator can distant surveillance shooting picture.
Further, described power set are provided with protective cover, not only can effectively protect propeller and machineBody, and avoid the propeller of aircraft in flight course rotation to collide other objects, cause pendant out of controlMachine.
The utility model beneficial effect is against existing technologies: adopt GPS locator to set around circleAfter the heart and radius, aircraft is realized circuit, and in pitch of the laps process, flying to control device can constantly gather from GPSThe data of locator also ensure around attitude and running orbit by accurate calculating of processor; Fuselage is provided with fourHorn and four groups of power set, make that aircraft action is more flexible, balance, and operating characteristics is better.
Below in conjunction with the drawings and specific embodiments, the utility model is described further.
Brief description of the drawings
Fig. 1 is the structural representation of aircraft in the utility model preferred embodiment;
Fig. 2 is the structural representation of remote control equipment in the utility model preferred embodiment;
Fig. 3 is the frame diagram of the utility model preferred embodiment.
Detailed description of the invention
As Figure 1-3, in the utility model preferred embodiment adjustable point around remotely-piloted vehicle, compriseAircraft 1 and remote control equipment 2, described aircraft 1 comprises fuselage 11, is arranged on the power dress on fuselage 11Put 12 with filming apparatus 13, described power set 12 are made up of motor 121 and propeller 122, propeller122 are arranged on the clutch end of motor 121 rotatingly, and fuselage 11 is provided with four horns 14, described inPower set 12 are provided with four groups, and four groups of power set 12 are separately fixed at the end of four horns 14, described machineBody 11 is provided with GPS locator 15, the first dual-mode antenna 16, memory 17 and processor 18, described batTake the photograph device 13, power set 12, GPS locator 15, the first dual-mode antenna 16, memory 17 all with locateReason device 18 is electrically connected; Described remote control equipment 2 comprises the second dual-mode antenna 21, manipulation handle 22 and controller 23,Described the second dual-mode antenna 21, manipulation handle 22 are all electrically connected with controller 23.
After aircraft 1 takes off flight to the correct position of intending reference object, by remote control equipment 2 to aircraft 1Provide instruction and enter fixed point pitch of the laps pattern. First, remote control equipment 2 passes through the second dual-mode antenna 21 to aircraft1 sends and determines around the command signal in the center of circle, then, by manipulation handle 22 remotely-piloted vehicles 1 fly away from aroundCentral point is to distance around center of circle correct position, and remote control equipment 2 passes through the second dual-mode antenna 21 to 1, aircraftGo out to determine the command signal around radius, set after the center of circle and radius, aircraft 1 starts pitch of the laps, aroundIn circle process, aircraft 1 can constantly gather from the data of GPS locator 15 and by processor 18 essencesClose calculating ensures around attitude and running orbit.
Described remote control equipment 2 is provided with display unit 24, and display unit 24 is electrically connected with controller 23, aobviousShowing device 24 receives the photographic images of filming apparatus 13.
Described power set 12 are provided with protective cover 19.
The foregoing is only preferred embodiment of the present utility model, be not used for limiting enforcement of the present utility modelScope; Be all equivalents of doing according to claim scope of the present utility model, be of the present utility modelClaim scope covers.
Claims (5)
- Adjustable point around a remotely-piloted vehicle, comprise aircraft and remote control equipment, described aircraft bagDraw together fuselage, be arranged on power set and filming apparatus on fuselage, it is characterized in that, described fuselage is provided withGPS locator, the first dual-mode antenna, memory and processor, described filming apparatus, power set, GPSLocator, the first dual-mode antenna, memory are all electrically connected with processor; Described remote control equipment comprises the second receiptsSend out antenna, manipulation handle and controller, described the second dual-mode antenna, manipulation handle are all electrically connected with controller.
- As claimed in claim 1 adjustable point around remotely-piloted vehicle, it is characterized in that: described power dressPut by motor and propeller and form, propeller is arranged on the clutch end of motor rotatingly.
- As claimed in claim 1 adjustable point around remotely-piloted vehicle, it is characterized in that: described fuselage is establishedHave four horns, described power set are provided with four groups, and described four groups of power set are separately fixed at the end of four hornsEnd.
- As claimed in claim 1 adjustable point around remotely-piloted vehicle, it is characterized in that: described remote controlEquipment is provided with display unit, and display unit is electrically connected with controller.
- As described in claim 1-4 any one adjustable point around remotely-piloted vehicle, it is characterized in that:Described power set are provided with protective cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520650031.1U CN205239910U (en) | 2015-08-21 | 2015-08-21 | Remote control flight ware that can fix a point to encircle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520650031.1U CN205239910U (en) | 2015-08-21 | 2015-08-21 | Remote control flight ware that can fix a point to encircle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205239910U true CN205239910U (en) | 2016-05-18 |
Family
ID=55938978
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520650031.1U Expired - Fee Related CN205239910U (en) | 2015-08-21 | 2015-08-21 | Remote control flight ware that can fix a point to encircle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205239910U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947217A (en) * | 2016-05-23 | 2016-09-21 | 中山市捷信科技服务有限公司 | Remote control type agricultural chemical spraying aircraft |
| CN108128455A (en) * | 2017-11-30 | 2018-06-08 | 广州市华科尔科技股份有限公司 | A kind of multi-rotor unmanned aerial vehicle control method |
-
2015
- 2015-08-21 CN CN201520650031.1U patent/CN205239910U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947217A (en) * | 2016-05-23 | 2016-09-21 | 中山市捷信科技服务有限公司 | Remote control type agricultural chemical spraying aircraft |
| CN108128455A (en) * | 2017-11-30 | 2018-06-08 | 广州市华科尔科技股份有限公司 | A kind of multi-rotor unmanned aerial vehicle control method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6312178B2 (en) | Navigation system, method for evaluating state information of transport aircraft, and apparatus for evaluating state information of transport aircraft | |
| CN107438805B (en) | Unmanned aerial vehicle (UAV) control method and device | |
| CN105242685B (en) | A kind of accompanying flying unmanned plane system and method | |
| US9676480B2 (en) | Flying machine capable of blocking light autonomously | |
| WO2018209702A1 (en) | Method for controlling unmanned aerial vehicle, unmanned aerial vehicle and machine-readable storage medium | |
| EP3345832B1 (en) | Unmanned aerial vehicle and method for controlling the same | |
| CN104155981B (en) | A kind of on-air radio pyroelectric monitor system of ground remote control based on many rotors robot | |
| WO2016138687A1 (en) | Control system, terminal and airborne flight control system of multi-rotor craft | |
| CN110692027A (en) | System and method for providing easy-to-use release and automatic positioning of drone applications | |
| CN201217501Y (en) | Suspending type aviation camera shooting self-determination aircraft system | |
| CN104808680A (en) | Multi-rotor flight shooting device | |
| CN105759833A (en) | Immersive unmanned aerial vehicle driving flight system | |
| CN106347694B (en) | A kind of Information Acquisition System based near space floating platform | |
| CN112326686A (en) | Unmanned aerial vehicle intelligent cruise pavement disease detection method, unmanned aerial vehicle and detection system | |
| CN204297114U (en) | A kind of can high-altitude location four-axle aircraft | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN110658840A (en) | Autonomous navigation obstacle avoidance method and device for multi-rotor unmanned aerial vehicle | |
| WO2017113648A1 (en) | Somatosensory remote controller, somatosensory remote control flight system and method, and remote control method | |
| CN104166054A (en) | Air radio monitoring system based on multi-rotor robot | |
| CN106628180A (en) | Flight airdropping device and airdropping method thereof | |
| KR102160734B1 (en) | Image taking system using wireless rechargeable drones | |
| CN106483980A (en) | A kind of unmanned plane follows the control method of flight, apparatus and system | |
| CN203865010U (en) | Navigation aircraft capable of achieving automatic tracking, video recognition and intelligent aerial photographing | |
| CN205239910U (en) | Remote control flight ware that can fix a point to encircle | |
| CN108910040A (en) | Mobile device aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 515800 Phoenix industry, Chenghai District, Guangdong, Shantou Patentee after: GUANGDONG CHENGXING UNMANNED AERIAL VEHICLE COMPANY LIMITED Address before: 515800 Phoenix industry, Chenghai District, Guangdong, Shantou Patentee before: Guangdong Chengxing Modelairplane Science Company Limted |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160518 Termination date: 20190821 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |