CN106354154A - Flying limiting system for geographic position of unmanned aerial vehicle - Google Patents
Flying limiting system for geographic position of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106354154A CN106354154A CN201610913309.9A CN201610913309A CN106354154A CN 106354154 A CN106354154 A CN 106354154A CN 201610913309 A CN201610913309 A CN 201610913309A CN 106354154 A CN106354154 A CN 106354154A
- Authority
- CN
- China
- Prior art keywords
- flying
- module
- central control
- control module
- unmanned plane
- 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.)
- Pending
Links
- 238000005516 engineering process Methods 0.000 description 3
- 238000005192 partition Methods 0.000 description 2
- 238000013316 zoning Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Alarm Systems (AREA)
Abstract
The invention discloses a flying limiting system for the geographic position of an unmanned aerial vehicle. The flying limiting system comprises a central control module, a man-machine interface system, an alarm module and a protection response module, wherein the central control module is in two-way connection with the man-machine interface system; the alarm module is in two-way connection with the man-machine interface system; the protection response module is in two-way connection with the central control module; the man-machine interface system consists of an area division system and a mode selection system; and the area division system comprises a conventional spherical system and a self-definition system. The flying limiting system disclosed by the invention has the advantages that self division for the flying limiting area is realized, the controllability for the flying area is guaranteed and the unnecessary flying loss is avoided.
Description
Technical field
The invention belongs to the winged technical field of unmanned plane region limit, specifically, the present invention relates to a kind of unmanned plane geography position
Put limit and fly system.
Background technology
Present unmanned plane in technical grade operation, usually occurs flight range inaccurate the flying into of positioning should not be flown into
Geographical position, causes unnecessary fault；In consumer level player's flight, also often occur flying out in zone of control.
It is substantially can only to determine half warp it is impossible to random oneself zoning, in addition that present unmanned plane position limit flies technology
Present technology is substantially flown in radius region from but is flown not going out, and the unmanned plane not enabling outside flies not enter
Certain region.
Content of the invention
The present invention provide a kind of unmanned plane geographical position limit to fly system it is therefore an objective to realize voluntarily dividing restricted area domain it is ensured that
The controllability of flight range, it is to avoid unnecessary flight loss.
To achieve these goals, the technical scheme that the present invention takes is: a kind of unmanned plane geographical position limit flies system, bag
Include central control module, human-computer interface system, alarm module and protection respond module, wherein said central control module with man-machine
Interface system is bi-directionally connected, and described alarm module and human-computer interface system are bi-directionally connected, and described protection respond module is controlled with central authorities
Molding block is bi-directionally connected.
Preferably, described human-computer interface system is made up of area dividing system and model selection system.
Preferably, described area dividing system includes conventional ball system and self-defined system.
The present invention seeks to realizing voluntarily dividing restricted area domain it is ensured that the controllability of flight range, it is to avoid unnecessary flies
Row loss, flies system to unmanned plane geographical position limit and has done brand-new design, the beneficial effect using above technical scheme is: be logical
Cross the conventional ball system in the area dividing system of human-computer interface system and self-defined system, realize conventional ball region and appoint
The division of meaning shape area；By model selection system, the switching of clearance inside and outside feasible region；By alarm module and guarantor
Shield respond module is it is achieved that report to the police not only by alarm module and take protection by protection respond module when near zone boundary
Measure.
Brief description
Fig. 1 is that unmanned plane geographical position limit flies systematic schematic diagram；
Specific embodiment
Below against accompanying drawing, by the description to embodiment, the specific embodiment of the present invention is made further details of
Illustrate it is therefore an objective to help those skilled in the art to have more complete, accurate and deep reason to the design of the present invention, technical scheme
Solution, and contribute to its enforcement.
As shown in figure 1, the present invention is a kind of unmanned plane geographical position limit flies system, it is used to realize voluntarily dividing restricted area
Domain is it is ensured that the controllability of flight range, it is to avoid unnecessary flight loss.
Specifically, as shown in figure 1, including central control module, human-computer interface system, alarm module and protection response mould
Block, wherein said central control module and human-computer interface system are bi-directionally connected, and described alarm module is two-way with human-computer interface system
Connect, described protection respond module is bi-directionally connected with central control module.Described human-computer interface system by area dividing system and
Model selection system forms.Described area dividing system includes conventional ball system and self-defined system.
With specific embodiment, specific works mode is illustrated below:
When we are when with unmanned plane execution task, according to specific operating environment, first pass through in human-computer interface system
Model selection system, selection is or to be flown institute's partition is overseas in institute's partition domain, then passes through human-computer interface system
In area dividing system zoning, the conventional ball system in area dividing system and self-defined system, realize conventional ball
Shape region and the division of arbitrary shaped region；Unmanned plane flies in the region dividing under the control of central control module, when
When unmanned plane flies nearly changed border, by alarm module and protection respond module it is achieved that not only leading to when near zone boundary
Cross alarm module to report to the police and take protective measure by protection respond module.
Above in association with accompanying drawing, the present invention is exemplarily described it is clear that the present invention implements is not subject to above-mentioned side
The restriction of formula, as long as employ the improvement of the various unsubstantialities that method of the present invention design is carried out with technical scheme；Or not
Improved, the above-mentioned design of the present invention and technical scheme are directly applied to other occasions, all in protection scope of the present invention
Within.
Claims (3)
1. a kind of unmanned plane geographical position limit fly system it is characterised in that: include central control module, human-computer interface system, report
Alert module and protection respond module, wherein said central control module and human-computer interface system are bi-directionally connected, described alarm module
It is bi-directionally connected with human-computer interface system, described protection respond module is bi-directionally connected with central control module.
2. a kind of unmanned plane geographical position according to claim 1 limit fly system it is characterised in that: described man machine interface system
System is made up of area dividing system and model selection system.
3. a kind of unmanned plane geographical position according to claim 2 limit fly system it is characterised in that: described region division system
System includes conventional ball system and self-defined system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610913309.9A CN106354154A (en) | 2016-10-19 | 2016-10-19 | Flying limiting system for geographic position of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610913309.9A CN106354154A (en) | 2016-10-19 | 2016-10-19 | Flying limiting system for geographic position of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106354154A true CN106354154A (en) | 2017-01-25 |
Family
ID=57864016
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610913309.9A Pending CN106354154A (en) | 2016-10-19 | 2016-10-19 | Flying limiting system for geographic position of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106354154A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104834307A (en) * | 2015-04-23 | 2015-08-12 | 杨珊珊 | Control method and control device of unmanned aerial vehicle |
| CN104881023A (en) * | 2015-04-23 | 2015-09-02 | 杨珊珊 | Control method of multi-rotor type aircraft, and multi-rotor type aircraft |
| US20150254988A1 (en) * | 2014-04-17 | 2015-09-10 | SZ DJI Technology Co., Ltd | Flight control for flight-restricted regions |
| CN106019309A (en) * | 2016-08-16 | 2016-10-12 | 广东容祺智能科技有限公司 | Unmanned-plane-based laser radar obstacle avoidance system and method |
-
2016
- 2016-10-19 CN CN201610913309.9A patent/CN106354154A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150254988A1 (en) * | 2014-04-17 | 2015-09-10 | SZ DJI Technology Co., Ltd | Flight control for flight-restricted regions |
| CN104834307A (en) * | 2015-04-23 | 2015-08-12 | 杨珊珊 | Control method and control device of unmanned aerial vehicle |
| CN104881023A (en) * | 2015-04-23 | 2015-09-02 | 杨珊珊 | Control method of multi-rotor type aircraft, and multi-rotor type aircraft |
| CN106019309A (en) * | 2016-08-16 | 2016-10-12 | 广东容祺智能科技有限公司 | Unmanned-plane-based laser radar obstacle avoidance system and method |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170125 |