CN106325286A - Method and system for adjusting flight height of unmanned aerial vehicle based on electric quantity - Google Patents
Method and system for adjusting flight height of unmanned aerial vehicle based on electric quantity Download PDFInfo
- Publication number
- CN106325286A CN106325286A CN201610685268.2A CN201610685268A CN106325286A CN 106325286 A CN106325286 A CN 106325286A CN 201610685268 A CN201610685268 A CN 201610685268A CN 106325286 A CN106325286 A CN 106325286A
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- CN
- China
- Prior art keywords
- unmanned plane
- dump energy
- altitude range
- electric quantity
- threshold value
- 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.)
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/042—Control of altitude or depth specially adapted for aircraft
Abstract
The invention provides a method and system for adjusting the flight height of an unmanned aerial vehicle based on electric quantity. The method includes the following steps that: the residual electric quantity of the unmanned aerial vehicle is detected; whether the residual electric quantity is lower than a set threshold value is judged; and when the residual electric quantity is lower than the set threshold value, and the height of the unmanned aerial vehicle is controlled to be a height range corresponding to the residual electric quantity. The method and system provided by the technical schemes of the invention have the advantage of high user experience.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of method based on electricity adjustment unmanned plane during flying height and be
System.
Background technology
The most unpiloted aircraft of unmanned plane, owing to it is without driving cabin, so its volume can be accomplished the least, existing
Unmanned plane generally battery is powered, and existing unmanned plane cannot cause electricity according to the electricity of battery to being highly adjusted
Loss is big, affects the experience of user.
Summary of the invention
A kind of method adjusting unmanned plane during flying height based on electricity is provided, which solves prior art user Experience Degree low
Shortcoming.
On the one hand, it is provided that a kind of method adjusting unmanned plane during flying height based on electricity, described method comprises the steps:
The dump energy of detection unmanned plane；
Judge that whether dump energy is less than setting threshold value；
When dump energy is less than when setting threshold value, control unmanned plane height in the altitude range that this dump energy is corresponding.
Optionally, described method also includes:
This altitude range is sent to user.
Optionally, described method also includes:
Receive user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
Second aspect, it is provided that a kind of system adjusting unmanned plane during flying height based on electricity, described system includes:
Detector unit, for detecting the dump energy of unmanned plane；
Judging unit, is used for judging that whether dump energy is less than setting threshold value；
Control unit, for controlling unmanned plane height in the altitude range that this dump energy is corresponding.
Optionally, described system also includes:
Transmitting element, for being sent to user by this altitude range.
Optionally, described system also includes:
Adjustment unit, for receiving user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
The dump energy of the technical scheme detection unmanned plane that the specific embodiment of the invention provides, when dump energy is less than setting
When determining threshold value, control unmanned plane height is in the altitude range that this dump energy is corresponding, so it has improves Consumer's Experience
Advantage.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
In having technology to describe, the required accompanying drawing used is briefly described, it should be apparent that, the accompanying drawing in describing below is only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to
Other accompanying drawing is obtained according to these accompanying drawings.
The flow chart of a kind of method adjusting unmanned plane during flying height based on electricity that Fig. 1 provides for the present invention；
The structure chart of a kind of system adjusting unmanned plane during flying height based on electricity that Fig. 2 provides for the present invention.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.Based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under not making creative work premise
Embodiment, broadly falls into the scope of protection of the invention.
Unmanned plane during flying is adjusted for the one that the present invention the first better embodiment provides based on electricity high refering to Fig. 1, Fig. 1
The flow chart of the method for degree, the method is completed by robot, and the method is as it is shown in figure 1, comprise the steps:
Step S101, the dump energy of detection unmanned plane；
Step S102, judge that dump energy is whether less than setting threshold value；
Step S103, when dump energy is less than when setting threshold value, control unmanned plane height at height corresponding to this dump energy
In the range of degree.
The dump energy of the technical scheme detection unmanned plane that the specific embodiment of the invention provides, when dump energy is less than setting
When determining threshold value, control unmanned plane height is in the altitude range that this dump energy is corresponding, so it has improves Consumer's Experience
Advantage.
Optionally, said method can also include after step s 103:
This altitude range is sent to user.
Optionally, said method can also include after step s 103:
Receive user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
Unmanned plane during flying is adjusted for the one that the present invention the second better embodiment provides based on electricity high refering to Fig. 2, Fig. 2
The system of degree, this system includes:
Detector unit 201, for detecting the dump energy of unmanned plane；
Judging unit 202, is used for judging that whether dump energy is less than setting threshold value；
Control unit 203, for controlling unmanned plane height in the altitude range that this dump energy is corresponding.
The dump energy of the technical scheme detection unmanned plane that the specific embodiment of the invention provides, when dump energy is less than setting
When determining threshold value, control unmanned plane height is in the altitude range that this dump energy is corresponding, so it has improves Consumer's Experience
Advantage.
Optionally, said system can also include:
Transmitting element 204, for being sent to user by this altitude range.
Optionally, said system can also include:
Adjustment unit 205, for receiving user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
It should be noted that for aforesaid each method embodiment or embodiment, in order to be briefly described, therefore by its all table
Stating as a series of combination of actions, but those skilled in the art should know, the present invention is not by described sequence of movement
Restriction, because of according to the present invention, some step can use other orders or carry out simultaneously.Secondly, people in the art
Member also should know, embodiment described in the specification or embodiment belong to preferred embodiment, involved action and list
Necessary to the unit not necessarily present invention.
In the above-described embodiments, the description to each embodiment all emphasizes particularly on different fields, and does not has the portion described in detail in certain embodiment
Point, may refer to the associated description of other embodiments.
Step in embodiment of the present invention method can carry out order according to actual needs and adjust, merges and delete.
Unit in embodiment of the present invention device can merge according to actual needs, divides and delete.This area
The feature of the different embodiments described in this specification and different embodiment can be combined or combine by technical staff.
Through the above description of the embodiments, those skilled in the art it can be understood that to the present invention permissible
Realize with hardware, or firmware realizes, or combinations thereof mode realizes.When implemented in software, can be by above-mentioned functions
It is stored in computer-readable medium or is transmitted as the one or more instructions on computer-readable medium or code.Meter
Calculation machine computer-readable recording medium includes computer-readable storage medium and communication media, and wherein communication media includes being easy to from a place to another
The individual local any medium transmitting computer program.Storage medium can be any usable medium that computer can access.With
As a example by this but be not limited to: computer-readable medium can include random access memory (Random Access Memory,
RAM), read only memory (Read-Only Memory, ROM), EEPROM (Electrically
Erasable Programmable Read-Only Memory, EEPROM), read-only optical disc (Compact Disc Read-
Only Memory, CD-ROM) or other optical disc storage, magnetic disk storage medium or other magnetic storage apparatus or can be used in
Carry or store and there is instruction or the desired program code of data structure form can be by any other of computer access
Medium.In addition.Any connection can be suitable become computer-readable medium.Such as, if software is to use coaxial cable, light
Fine optical cable, twisted-pair feeder, Digital Subscriber Line (Digital Subscriber Line, DSL) or such as infrared ray, radio and
The wireless technology of microwave etc from website, server or other remote source, then coaxial cable, optical fiber cable, double
The wireless technology of twisted wire, DSL or such as infrared ray, wireless and microwave etc be included in affiliated medium fixing in.Such as this
Bright used, dish (Disk) and dish (disc) include compress laser disc (CD), laser dish, laser disc, Digital Versatile Disc (DVD),
Floppy disk and Blu-ray Disc, the duplication data of the usual magnetic of its mid-game, dish then carrys out the duplication data of optics with laser.Group above
Close within should also be as being included in the protection domain of computer-readable medium.
In a word, the foregoing is only the preferred embodiment of technical solution of the present invention, be not intended to limit the present invention's
Protection domain.All within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. made, should be included in
Within protection scope of the present invention.
Claims (6)
1. the method adjusting unmanned plane during flying height based on electricity, it is characterised in that described method comprises the steps:
The dump energy of detection unmanned plane；
Judge that whether dump energy is less than setting threshold value；
When dump energy is less than when setting threshold value, control unmanned plane height in the altitude range that this dump energy is corresponding.
Method the most according to claim 1, it is characterised in that described method also includes:
This altitude range is sent to user.
Method the most according to claim 1, it is characterised in that described method also includes:
Receive user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
4. the system adjusting unmanned plane during flying height based on electricity, it is characterised in that described system includes:
Detector unit, for detecting the dump energy of unmanned plane；
Judging unit, is used for judging that whether dump energy is less than setting threshold value；
Control unit, for controlling unmanned plane height in the altitude range that this dump energy is corresponding.
System the most according to claim 4, it is characterised in that described system also includes:
Transmitting element, for being sent to user by this altitude range.
System the most according to claim 4, it is characterised in that described system also includes:
Adjustment unit, for receiving user's feedback to this altitude range, according to this altitude range of this feedback adjustment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610685268.2A CN106325286A (en) | 2016-08-17 | 2016-08-17 | Method and system for adjusting flight height of unmanned aerial vehicle based on electric quantity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610685268.2A CN106325286A (en) | 2016-08-17 | 2016-08-17 | Method and system for adjusting flight height of unmanned aerial vehicle based on electric quantity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106325286A true CN106325286A (en) | 2017-01-11 |
Family
ID=57744065
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610685268.2A Pending CN106325286A (en) | 2016-08-17 | 2016-08-17 | Method and system for adjusting flight height of unmanned aerial vehicle based on electric quantity |
Country Status (1)
| Country | Link |
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| CN (1) | CN106325286A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106707192A (en) * | 2017-01-23 | 2017-05-24 | 深圳市哈威飞行科技有限公司 | Aircraft safety detection management device and safety control system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102107702A (en) * | 2010-12-27 | 2011-06-29 | 上海鹄展大丰电动自行车制造有限公司 | Electric motor car driving computer device |
| CN202106921U (en) * | 2011-04-02 | 2012-01-11 | 刘鸿滨 | Driving computer control device suitable for electric vehicle |
| CN202460124U (en) * | 2012-03-16 | 2012-10-03 | 罗之洪 | Remote control aircraft with state monitoring function |
| US20140129059A1 (en) * | 2012-05-17 | 2014-05-08 | The Boeing Company | Method and apparatus for extending the operation of an unmanned aerial vehicle |
| CN104166355A (en) * | 2014-07-16 | 2014-11-26 | 深圳市大疆创新科技有限公司 | Electric unmanned aerial vehicle and intelligent electric quantity protection method |
| CN104881041A (en) * | 2015-05-27 | 2015-09-02 | 深圳市高巨创新科技开发有限公司 | Unmanned aircraft electric quantity early warning method and device |
| CN205353767U (en) * | 2015-11-24 | 2016-06-29 | 余江 | Unmanned aerial vehicle |
-
2016
- 2016-08-17 CN CN201610685268.2A patent/CN106325286A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102107702A (en) * | 2010-12-27 | 2011-06-29 | 上海鹄展大丰电动自行车制造有限公司 | Electric motor car driving computer device |
| CN202106921U (en) * | 2011-04-02 | 2012-01-11 | 刘鸿滨 | Driving computer control device suitable for electric vehicle |
| CN202460124U (en) * | 2012-03-16 | 2012-10-03 | 罗之洪 | Remote control aircraft with state monitoring function |
| US20140129059A1 (en) * | 2012-05-17 | 2014-05-08 | The Boeing Company | Method and apparatus for extending the operation of an unmanned aerial vehicle |
| CN104166355A (en) * | 2014-07-16 | 2014-11-26 | 深圳市大疆创新科技有限公司 | Electric unmanned aerial vehicle and intelligent electric quantity protection method |
| CN104881041A (en) * | 2015-05-27 | 2015-09-02 | 深圳市高巨创新科技开发有限公司 | Unmanned aircraft electric quantity early warning method and device |
| CN205353767U (en) * | 2015-11-24 | 2016-06-29 | 余江 | Unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106707192A (en) * | 2017-01-23 | 2017-05-24 | 深圳市哈威飞行科技有限公司 | Aircraft safety detection management device and safety control system |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170111 |
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