CN106081131A - The control method of electric moter voltage and system in unmanned plane - Google Patents
The control method of electric moter voltage and system in unmanned plane Download PDFInfo
- Publication number
- CN106081131A CN106081131A CN201610682539.9A CN201610682539A CN106081131A CN 106081131 A CN106081131 A CN 106081131A CN 201610682539 A CN201610682539 A CN 201610682539A CN 106081131 A CN106081131 A CN 106081131A
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- Prior art keywords
- unmanned plane
- dump energy
- current range
- threshold value
- moter voltage
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- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000001514 detection method Methods 0.000 claims description 6
- 230000008901 benefit Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 4
- 230000005611 electricity Effects 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000013307 optical fiber Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D2221/00—Electric power distribution systems onboard aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention provides control method and the system of electric moter voltage in a kind of unmanned plane, described method comprises the steps: to detect the dump energy of 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 electric current in the current range that this dump energy is corresponding.The technical scheme that the present invention provides has the advantage that user experience is high.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to control method and the system of electric moter voltage in a kind of unmanned plane.
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 electric current cannot be adjusted by existing unmanned plane according to the electricity of battery, causes electricity
Loss is big, affects the experience of user.
Summary of the invention
The control method of electric moter voltage in a kind of unmanned plane is provided, which solves low the lacking of prior art user Experience Degree
Point.
On the one hand, it is provided that the control method of electric moter voltage in a kind of unmanned plane, 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 electric current in the current range that this dump energy is corresponding.
Optionally, described method also includes:
This current range is sent to user.
Optionally, described method also includes:
Receive user's feedback to this current range, according to this current range of this feedback adjustment.
Second aspect, it is provided that the control system of electric moter voltage in a kind of unmanned plane, 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 electric current in the current range that this dump energy is corresponding.
Optionally, described system also includes:
Transmitting element, for being sent to user by this current range.
Optionally, described system also includes:
Adjustment unit, for receiving user's feedback to this current range, according to this current 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 electric current is in the current 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 the control method of electric moter voltage in a kind of unmanned plane that Fig. 1 provides for the present invention；
The structure chart of the control system of electric moter voltage in a kind of unmanned plane 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.
The controlling party of electric moter voltage in a kind of unmanned plane provided for the present invention the first better embodiment refering to Fig. 1, Fig. 1
The flow chart of method, 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 electric current at electricity corresponding to this dump energy
In the range of stream.
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 electric current is in the current 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 current range is sent to user.
Optionally, said method can also include after step s 103:
Receive user's feedback to this current range, according to this current range of this feedback adjustment.
The control system of electric moter voltage in a kind of unmanned plane provided for the present invention the second better embodiment refering to Fig. 2, Fig. 2
System, 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 electric current in the current 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 electric current is in the current 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 current range.
Optionally, said system can also include:
Adjustment unit 205, for receiving user's feedback to this current range, according to this current 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 control method of electric moter voltage in a unmanned plane, 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 electric current in the current range that this dump energy is corresponding.
Method the most according to claim 1, it is characterised in that described method also includes:
This current 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 current range, according to this current range of this feedback adjustment.
4. the control system of electric moter voltage in a unmanned plane, 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 electric current in the current 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 current 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 current range, according to this current range of this feedback adjustment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610682539.9A CN106081131A (en) | 2016-08-17 | 2016-08-17 | The control method of electric moter voltage and system in unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610682539.9A CN106081131A (en) | 2016-08-17 | 2016-08-17 | The control method of electric moter voltage and system in unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106081131A true CN106081131A (en) | 2016-11-09 |
Family
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610682539.9A Pending CN106081131A (en) | 2016-08-17 | 2016-08-17 | The control method of electric moter voltage and system in unmanned plane |
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| CN (1) | CN106081131A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032418A1 (en) * | 2016-08-17 | 2018-02-22 | 张琬彬 | Method and system for controlling unmanned aerial vehicle motor current according to power level |
| WO2018032419A1 (en) * | 2016-08-17 | 2018-02-22 | 张琬彬 | Method and system for controlling unmanned aerial vehicle internal motor voltage |
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| 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 CN201610682539.9A patent/CN106081131A/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 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2018032418A1 (en) * | 2016-08-17 | 2018-02-22 | 张琬彬 | Method and system for controlling unmanned aerial vehicle motor current according to power level |
| WO2018032419A1 (en) * | 2016-08-17 | 2018-02-22 | 张琬彬 | Method and system for controlling unmanned aerial vehicle internal motor voltage |
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Application publication date: 20161109 |
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