CN205221112U - Unmanned aerial vehicle system - Google Patents
Unmanned aerial vehicle system Download PDFInfo
- Publication number
- CN205221112U CN205221112U CN201520841018.4U CN201520841018U CN205221112U CN 205221112 U CN205221112 U CN 205221112U CN 201520841018 U CN201520841018 U CN 201520841018U CN 205221112 U CN205221112 U CN 205221112U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- communication module
- aerial vehicle
- unmanned aerial
- wireless communication
- 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 discloses an unmanned aerial vehicle system, including unmanned aerial vehicle and ground station, unmanned aerial vehicle and ground station wireless communication, the last wireless communication module that installs of unmanned aerial vehicle installs wireless communication module on the ground station, unmanned aerial vehicle's the wireless communication module and the wireless communication module of ground station pass through the wireless network communication. The utility model provides an unmanned aerial vehicle system has increased wireless communication module on unmanned aerial vehicle and ground station, unmanned aerial vehicle's wireless communication module with the wireless communication module of ground station passes through the wireless network communication, and at the within range that unmanned aerial vehicle and the unable direct communication of ground station just can cover at wireless network, unmanned aerial vehicle and ground station also can carry out the communication through wireless network to increased the communication context of system, reduced blind the flying of aircraft and the potential safety hazard that exists, solved the condition that the massif blocks to a certain extent under unmanned aerial vehicle can not receive the signal of ground station and have the greatly problem of potential safety hazard.
Description
Technical field
The utility model relates to flight equipment field, especially a kind of Unmanned Aircraft Systems (UAS).
Background technology
Unmanned plane is the abbreviation of robot airplane, along with the development and application field of science and technology is more and more extensive, especially in the search and rescue process of disaster, substantially increases the time of search and rescue, thus becomes not replaceable instrument.
Existing Unmanned Aircraft Systems (UAS) completes communication function by unmanned plane and the direct wireless telecommunications of earth station, this system communication distance is shorter, and unmanned plane boat flies operation and often exceeds this distance, blindly can only fly, there is greatly potential safety hazard like this, in addition, when there being massif to stop during operation, because massif stops, unmanned plane can not receive the signal of earth station yet, thus there is greatly potential safety hazard.
Summary of the invention
For this reason, the utility model proposes a kind of new Unmanned Aircraft Systems (UAS) at least partially that can solve the problem.
According to an aspect of the present utility model, provide a kind of Unmanned Aircraft Systems (UAS), comprise unmanned plane and earth station, described unmanned plane and earth station wireless telecommunications; Described unmanned plane is provided with wireless communication module, described earth station is provided with wireless communication module, the wireless communication module of described unmanned plane and the wireless communication module of described earth station pass through wireless network communication.
Optionally, described unmanned plane comprises the first unmanned plane and the second unmanned plane, and described first unmanned plane is provided with repeater station, described second unmanned plane and earth station respectively with described repeater station wireless telecommunications.
Optionally, described second unmanned plane is provided with satellite communication module, described earth station is provided with satellite communication module, the satellite communication module of described second unmanned plane and the satellite communication module of described earth station pass through satellite wireless communication.
Optionally, the quantity of described second unmanned plane is multiple stage.
The Unmanned Aircraft Systems (UAS) that the utility model provides, unmanned plane and earth station add wireless communication module, the wireless communication module of unmanned plane and the wireless communication module of described earth station pass through wireless network communication, cannot Direct Communication and in the scope that wireless network can cover at unmanned plane and earth station, unmanned plane and earth station also can carry out communication by wireless network, thus add the communication context of system, reduce blind the flying of aircraft and the potential safety hazard existed, to some extent solve unmanned plane when massif stops do not receive the signal of earth station and there is the problem of greatly potential safety hazard.
Accompanying drawing explanation
By reading hereafter detailed description of the preferred embodiment, various other advantage and benefit will become cheer and bright for those of ordinary skill in the art.Accompanying drawing only for illustrating the object of preferred implementation, and is not thought restriction of the present utility model.And in whole accompanying drawing, represent identical parts by identical reference symbol.Wherein in the accompanying drawings, the multiple identical parts of alphabetic flag instruction after reference number, when making a general reference these parts, by its last alphabetic flag of omission.In the accompanying drawings:
The structural representation of a kind of Unmanned Aircraft Systems (UAS) that Fig. 1 the utility model provides;
The structural representation of a kind of Unmanned Aircraft Systems (UAS) that Fig. 2 the utility model provides;
The structural representation of a kind of Unmanned Aircraft Systems (UAS) that Fig. 3 the utility model provides;
Wherein, 101, unmanned plane; 102, earth station; 103, the wireless communication module of unmanned plane; 104, the wireless communication module of earth station; 105, the first unmanned plane 106, second unmanned plane; 107, repeater station; 108, the satellite communication module of the second unmanned plane; 109, the satellite communication module of earth station.
Detailed description of the invention
Below in conjunction with accompanying drawing and concrete embodiment, the utility model will be further described.
Provide a kind of Unmanned Aircraft Systems (UAS) according to advantage of the present utility model, see Fig. 1, comprise unmanned plane 101 and earth station 102, described unmanned plane 101 and earth station 102 wireless telecommunications; Described unmanned plane is provided with wireless communication module, described earth station is provided with wireless communication module, the installation of wireless communication module is the technology that those skilled in the art know, do not repeating, the wireless communication module 103 of described unmanned plane passes through wireless network communication with the wireless communication module 104 of described earth station herein.
The Unmanned Aircraft Systems (UAS) that the utility model provides, unmanned plane and earth station add wireless communication module, the wireless communication module of unmanned plane and the wireless communication module of described earth station pass through wireless network communication, cannot Direct Communication and in the scope that wireless network can cover at unmanned plane and earth station, unmanned plane and earth station also can carry out communication by wireless network, thus add the communication context of system, reduce blind the flying of aircraft and the potential safety hazard existed, to some extent solve unmanned plane when massif stops do not receive the signal of earth station and there is the problem of greatly potential safety hazard.
Although the scope that wireless network covers is more and more wider, but also there is the place do not covered, or time out of order, like this, the wireless network module of installation will not have effect, for this reason, unmanned plane is divided into the first unmanned plane and the second unmanned plane, see Fig. 2, described first unmanned plane 105 is provided with repeater station 107, described second unmanned plane 106 and earth station 102 respectively with the wireless telecommunications of described repeater station 107.It should be noted that, the first unmanned plane and the second unmanned plane are all unmanned planes, just it are named so for convenience of description.During use, the first unmanned plane and the second unmanned plane all with the scope of earth station communication in or can work independently in the scope that wireless network covers; Except this situation, when needing the situation of increase communication distance or having massif to stop, first unmanned plane and the second unmanned plane can be with the use of: when not having massif to stop, first unmanned plane can be positioned at the intermediate flight of the second unmanned plane and earth station, second unmanned plane passes through repeater station and the earth station communication of the first unmanned plane, greatly can increase the efficient range of communication like this, reduce blind situation about flying and occur, thus reduce potential safety hazard; When there being massif to stop, first unmanned plane can be positioned at above the second unmanned plane and do not flown by the place stopped or spiral, as the transfer of the second unmanned plane and earth station communication, thus actv. solves the second unmanned plane and does not receive the signal of earth station and there is the problem of potential safety hazard further.
Unmanned Aircraft Systems (UAS) is in the process of work, first nobody also machine have fault unavoidably, or repeater station has problem etc. to cause repeater station not play a role thus causes the second unmanned plane to have potential safety hazard, for this reason, described second unmanned plane is provided with satellite communication module, see Fig. 3, described earth station is provided with satellite communication module, the satellite communication module 108 of described second unmanned plane passes through satellite wireless communication with the satellite communication module 109 of described earth station, the installation of communication module is the technology that those skilled in the art know, and is not repeating herein.Like this, the second unmanned plane and earth station can pass through satellite 110 communication, further ensure its safety.
It should be noted that, the quantity of above-mentioned second unmanned plane can be multiple stage, and like this, multiple stage second unmanned plane as transfer, improves the degree of utilization of the first unmanned plane with first unmanned plane.Certainly, the second unmanned plane also can install repeater station, can also can cooperatively interact by every two the second unmanned planes like this, and and the first unmanned plane also can cooperatively interact, if desired, the work of replacement first unmanned plane can be used for; First unmanned plane also can install satellite communication module and wireless communication module, mutually replace work with the second unmanned plane.
It should be noted, above-described embodiment is described the utility model instead of limits the utility model, and those skilled in the art can design alternative embodiment when not departing from the scope of claims.In the claims, any reference symbol between bracket should be configured to limitations on claims.Word " comprises " not to be got rid of existence and does not arrange element in the claims or step.Word "a" or "an" before being positioned at element is not got rid of and be there is multiple such element.The utility model can by means of including the hardware of some different elements and realizing by means of the computing machine of suitably programming.In the unit claim listing some devices, several in these devices can be carry out imbody by same hardware branch.Word first, second and third-class use do not represent any order.Can be title by these word explanations.
Claims (4)
1. a Unmanned Aircraft Systems (UAS), is characterized in that, comprises unmanned plane and earth station, described unmanned plane and described earth station wireless telecommunications;
Described unmanned plane is provided with wireless communication module, described earth station is provided with wireless communication module, the wireless communication module of described unmanned plane and the wireless communication module of described earth station pass through wireless network communication.
2. Unmanned Aircraft Systems (UAS) according to claim 1, is characterized in that, described unmanned plane comprises the first unmanned plane and the second unmanned plane, and described first unmanned plane is provided with repeater station, described second unmanned plane and earth station respectively with described repeater station wireless telecommunications.
3. Unmanned Aircraft Systems (UAS) according to claim 2, it is characterized in that, described second unmanned plane is provided with satellite communication module, described earth station is provided with satellite communication module, the satellite communication module of described second unmanned plane and the satellite communication module of described earth station pass through satellite wireless communication.
4. Unmanned Aircraft Systems (UAS) according to claim 3, is characterized in that, the quantity of described second unmanned plane is multiple stage.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520841018.4U CN205221112U (en) | 2015-10-27 | 2015-10-27 | Unmanned aerial vehicle system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520841018.4U CN205221112U (en) | 2015-10-27 | 2015-10-27 | Unmanned aerial vehicle system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205221112U true CN205221112U (en) | 2016-05-11 |
Family
ID=55896194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201520841018.4U Expired - Fee Related CN205221112U (en) | 2015-10-27 | 2015-10-27 | Unmanned aerial vehicle system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205221112U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019041633A1 (en) * | 2017-08-28 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Communication relay method, relay aerial vehicle, program, and recording medium |
CN109891476A (en) * | 2016-11-04 | 2019-06-14 | 索尼公司 | Circuit, base station, method and recording medium |
-
2015
- 2015-10-27 CN CN201520841018.4U patent/CN205221112U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109891476A (en) * | 2016-11-04 | 2019-06-14 | 索尼公司 | Circuit, base station, method and recording medium |
WO2019041633A1 (en) * | 2017-08-28 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Communication relay method, relay aerial vehicle, program, and recording medium |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN205221126U (en) | Unmanned aerial vehicle system | |
WO2014077913A3 (en) | Determination of flight path for unmanned aircraft in event of in-flight contingency | |
US20140074321A1 (en) | Methods and systems for vehicle broadband connection to a data network | |
CN106354153A (en) | Unmanned aerial vehicle flight control method and device | |
CN202642096U (en) | Small-scale unmanned aerial vehicle, as well as onboard arresting gear, ground arresting gear and arresting system thereof | |
CN205221112U (en) | Unmanned aerial vehicle system | |
CN101714300A (en) | Unmanned plane flight collision avoidance method and device | |
CN205661674U (en) | Electric magnet positioning device that unmanned aerial vehicle descends on on -vehicle platform that rises and falls | |
EP2988456B1 (en) | Method and system to add and communicate with remote terminal addresses beyond a standard bus protocol | |
CN102183941A (en) | Civil-mobile-phone-network-based ultra-long-range unmanned aerial vehicle control system | |
CN106094874A (en) | Control the method for unmanned plane, controller and unmanned plane | |
CN111077818B (en) | Control box for aircraft data forwarding and transmitting control | |
CN112650279A (en) | Cloud flight management system and cloud flight management method for airplane | |
EP3327529B1 (en) | Control station for unmanned air vehicles and working procedure | |
AU2018264004B2 (en) | Method and apparatus for physical security over a powerline connection | |
CN106468775A (en) | Aircraft tracking and equipment and installation method | |
CN103901881A (en) | Device compatible with multiple test states for carrier rocket equivalent device system | |
CN202102301U (en) | Super long-range unmanned aerial vehicle control system based on civil mobile phone network | |
WO2019089597A1 (en) | Distributed aircraft recorder system | |
CN103869808B (en) | Carrier rocket simulator system based on distributed computing technology | |
DE102012200487A1 (en) | Onboard communication device and system for a cabin of a vehicle | |
CN106034162A (en) | Method, system and device for maintaining aircraft-mounted equipment | |
CN106330292A (en) | General vehicle satellite communication system and general vehicle satellite communication method | |
US9727689B2 (en) | System and method for wiring an aircraft | |
US20220352977A1 (en) | Communication module for transmission of aircraft data |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160511 Termination date: 20211027 |