CN107765189A - The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity - Google Patents
The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity Download PDFInfo
- Publication number
- CN107765189A CN107765189A CN201711286747.8A CN201711286747A CN107765189A CN 107765189 A CN107765189 A CN 107765189A CN 201711286747 A CN201711286747 A CN 201711286747A CN 107765189 A CN107765189 A CN 107765189A
- Authority
- CN
- China
- Prior art keywords
- lithium battery
- capacity
- aerial vehicle
- unmanned aerial
- rotor unmanned
- 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
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 title claims abstract description 56
- 229910052744 lithium Inorganic materials 0.000 title claims abstract description 56
- 238000001514 detection method Methods 0.000 title claims abstract description 28
- 238000000034 method Methods 0.000 title claims abstract description 22
- 238000005259 measurement Methods 0.000 claims description 6
- 238000013473 artificial intelligence Methods 0.000 claims description 3
- 238000004590 computer program Methods 0.000 claims description 3
- 230000010349 pulsation Effects 0.000 claims description 3
- 241000208340 Araliaceae Species 0.000 description 2
- 235000005035 Panax pseudoginseng ssp. pseudoginseng Nutrition 0.000 description 2
- 235000003140 Panax quinquefolius Nutrition 0.000 description 2
- 238000005183 dynamical system Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 235000008434 ginseng Nutrition 0.000 description 2
- 239000000686 essence Substances 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 241000894007 species Species 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/005—Testing of electric installations on transport means
- G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
- G01R31/367—Software therefor, e.g. for battery testing using modelling or look-up tables
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
- G01R31/392—Determining battery ageing or deterioration, e.g. state of health
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
- G01R31/396—Acquisition or processing of data for testing or for monitoring individual cells or groups of cells within a battery
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Tests Of Electric Status Of Batteries (AREA)
- Secondary Cells (AREA)
Abstract
The invention belongs to unmanned air vehicle technique field, discloses a kind of detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity, opens detection (charging) device of Universal lithium-cell capacity, control parameter is set according to tested battery.The tested battery pack of connector connection, opens controlling switch and starts working, arrival is automatically stopped work after imposing a condition.This data is uploaded into computer end by USB lines to be analyzed.The present invention can obtain detailed lithium battery discharge curve, and lithium battery various performance parameters, such as capacity, life-span, the ideal interval of battery discharge etc. are accurately analyzed according to curve.According to the performance parameter of lithium battery, lithium battery is used with can more rationally making, the use to gyroplane provides more sound assurance.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to a kind of multi-rotor unmanned aerial vehicle to be filled with the detection of lithium battery capacity
Electrographic recording system and method.
Background technology
Gyroplane be it is a kind of using autorotation to produce the rotary wing aircraft of lift, be between helicopter and aircraft
Aircraft;According to the motionless propeller equipped with varying number of species, there is VTOL, can low speed low-latitude flying, simple
Lightly, it is easy to the features such as hidden.In recent years, as the maturation of gyroplane items technology, gyroplane start by increasing
Pay attention to.For at present, gyroplane is mainly made up of dynamical system, control system, execution system and fuselage etc..It is current most absolutely
The dynamical system of several gyroplanes is all to use lithium battery as power resources.But also lack in the market to gyroplane institute
The instrument and equipment fully detected with the performance of lithium battery.Measured in the discharge parameter for lithium battery mainly by charger
Additional function complete.Because the major function of charger is charging, he can not provide a variety of discharge modes, can not remember
Record discharge curve.Overall merit can not be provided to battery.Measured now for the discharge parameter of lithium battery mainly by charger
Additional function complete, but charger can only provide some simple parameters, it is impossible to it is bent to provide the detailed electric discharge of lithium battery
Line, the performance of analysis lithium battery that can not be in detail.
In summary, the problem of prior art is present be:The discharge parameter for lithium battery, which measures, in the market is present
Charger can only provide simple parameter, it is impossible to provide the lithium battery detailed discharge curve, analysis lithium battery that can not be in detail
Performance.
The content of the invention
The problem of existing for prior art, the invention provides a kind of detection of multi-rotor unmanned aerial vehicle lithium battery capacity
Record of charging system and method.
The present invention is achieved in that a kind of full discharge parameter recording method of multi-rotor unmanned aerial vehicle lithium battery, described more
The full discharge parameter recording method of rotor wing unmanned aerial vehicle lithium battery includes:
Step 1, the detection charging device of Universal lithium-cell capacity is opened, control parameter is set according to tested battery;
Step 2, the tested battery pack of connector connection, opens controlling switch and starts working.Arrival stops automatically after imposing a condition
Only work.This data is uploaded into computer end by USB lines to be analyzed.
Step 3, computer end, by the comparison of database, are analyzed according to data using artificial intelligence.Accurately give
Go out the overall merit of tested battery pack.
Further, the multi-rotor unmanned aerial vehicle is inputted with the detection record of charging method computer of lithium battery capacity according to client
Battery parameter, started working after being confirmed by lithium battery detection mouth to battery size;
Computer program can start in electric discharge respectively, the time that is middle, closing on end respectively with 10 times of high currents, 5 times it is medium
Electric current carries out pulsation electric discharge and normal current electric discharge.And recording voltage and current curve;Total electric discharge is recorded after electric discharge terminates
Capacity;Provide the conclusion of this discharge capacity measurement.Program starts to control battery charging, and charging curve is drawn after being full of;Computer
Provide the measurement conclusion of this capacity;Obscured according to Voltage Drop curve and recording capacity with the respective record in database
Compare;Artificial intelligence program calculates efficiency for charge-discharge according to data.Provide the recommendation of preliminary electric discharge electric current and time;Calculate
The residual life of battery.
Another object of the present invention is to provide a kind of application multi-rotor unmanned aerial vehicle lithium battery full discharge parameter note
The unmanned plane of recording method.
The present invention can obtain detailed lithium battery discharge curve, and lithium battery properties ginseng is accurately analyzed according to curve
Number, such as capacity, life-span, the ideal interval of battery discharge etc..According to the performance parameter of lithium battery, can use with more rationally making
Lithium battery, the use to gyroplane provide more sound assurance.
Brief description of the drawings
Fig. 1 is the full discharge parameter recording device structure signal of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention
Figure;
Fig. 2 is the full discharge parameter tape deck backside structure of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention
Figure;
Fig. 3 is the full discharge parameter tape deck cabinet inside of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention
Structure chart;
In figure:1st, cabinet;2nd, keyboard;3rd, discharge resistance module;4th, radiator;5th, power switch;6th, display screen;7th, power supply
Interface;8th, USB interface;9th, lithium battery group electric discharge interface;10th, lithium battery detection interface;11st, radiator fan;12nd, CPU master control borads.
Fig. 4 is the full discharge parameter recording method flow chart of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to embodiments, to the present invention
It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to
Limit the present invention.
The present invention can provide lithium battery detailed discharge curve, and ginseng strong in detail is provided to analyze the performance of lithium battery
Number.
The application principle of the present invention is explained in detail below in conjunction with the accompanying drawings.
As shown in Figure 1-Figure 3, the full discharge parameter record bag of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention
Include:Cabinet 1, keyboard 2, discharge resistance module 3, radiator 4, power switch 5, display screen 6, power interface 7, USB interface 8, lithium
Battery power discharge interface 9, lithium battery detection interface 10, radiator fan 11, CPU master control borads 12.
CPU master control borads connection keyboard 2, display screen 6, USB interface 8, lithium battery detection interface 9, discharge resistance module 3;Put
Electric resistive module 3 connects lithium battery group electric discharge interface 9;USB interface 8 connects upper data computer.
As shown in figure 4, the full discharge parameter recording method bag of multi-rotor unmanned aerial vehicle lithium battery provided in an embodiment of the present invention
Include following steps:
S101:The detection charging device of Universal lithium-cell capacity is opened, control parameter is set according to tested battery;
S102:The tested battery pack of connector connection, opens controlling switch and starts working.Arrival is automatically stopped after imposing a condition
Work.This data is uploaded into computer end by USB lines to be analyzed.
S103:Computer end, by the comparison of database, is analyzed according to data using artificial intelligence.Accurately provide
The overall merit of tested battery pack.
The detection record of charging method computer of multi-rotor unmanned aerial vehicle lithium battery capacity provided in an embodiment of the present invention according to
The battery parameter of client's input, starts working after being confirmed by lithium battery detection mouth to battery size;
Computer program measures voltage to judge battery status and connect corresponding power resistance, divided according to battery setup parameter
Do not start in electric discharge, state that is middle, closing on end carries out pulsation electric discharge and just with 10 times of high currents, 5 times of medium currents respectively
Normal current discharge.And recording voltage and current curve;Total discharge capacity is recorded after electric discharge terminates;Provide this discharge capacity
The conclusion of measurement.Program starts to control battery charging, and charging curve is drawn after being full of;Computer provides the measurement knot of this capacity
By;It is compared according to Voltage Drop curve and recording capacity with the respective record in database and finds out corresponding data area;
Artificial intelligence program calculates efficiency for charge-discharge according to data.Provide the recommendation of preliminary electric discharge electric current and time;Calculate battery
Residual life.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
All any modification, equivalent and improvement made within refreshing and principle etc., should be included in the scope of the protection.
Claims (5)
1. a kind of detection record of charging method of multi-rotor unmanned aerial vehicle lithium battery capacity, it is characterised in that more rotors without
The man-machine detection record of charging method of lithium battery capacity includes:
The tested battery pack of connector connection, opens controlling switch and starts working;Arrival stops after imposing a condition;Pass through USB lines
This data is uploaded into computer end to be analyzed;
Computer end, by the comparison of database, is analyzed according to data using artificial intelligence;Accurately provide tested battery pack
Overall merit.
2. the detection record of charging method of multi-rotor unmanned aerial vehicle lithium battery capacity as claimed in claim 1, it is characterised in that
The detection record of charging method of the multi-rotor unmanned aerial vehicle lithium battery capacity also includes:
The detection charging device of Universal lithium-cell capacity is opened, control parameter is set according to tested battery.
3. the detection record of charging method of multi-rotor unmanned aerial vehicle lithium battery capacity as claimed in claim 1, it is characterised in that
The battery parameter that the detection record of charging method computer of the multi-rotor unmanned aerial vehicle lithium battery capacity inputs according to client, passes through
Lithium battery detection mouth is started working after confirming to battery size;
Computer program can start in electric discharge, be middle, closing on the time of end respectively with 10 times of high currents, 5 times of medium currents respectively
Carry out pulsation electric discharge and normal current electric discharge.And recording voltage and current curve;Total discharge capacity is recorded after electric discharge terminates;
Provide the conclusion of this discharge capacity measurement;Program starts to control battery charging, and charging curve is drawn after being full of;Computer provides this
The measurement conclusion of secondary capacity;Fuzzy compare is carried out with the respective record in database according to Voltage Drop curve and recording capacity;
Artificial intelligence program calculates efficiency for charge-discharge according to data;Provide the recommendation of preliminary electric discharge electric current and time;Calculate battery
Residual life.
4. a kind of more rotors of the detection record of charging method of multi-rotor unmanned aerial vehicle lithium battery capacity as claimed in claim 1 without
The man-machine detection record of charging device with lithium battery capacity, it is characterised in that the multi-rotor unmanned aerial vehicle lithium battery capacity
Detection record of charging device is provided with CPU master control borads;The CPU master control borads connect keyboard, display screen, USB by wire respectively
Interface, lithium battery detection interface, discharge resistance module;Discharge resistance module connects lithium battery group electric discharge interface by wire;USB
Interface connects upper data computer.
A kind of 5. more rotors of detection record of charging method using multi-rotor unmanned aerial vehicle lithium battery capacity described in claim 1
Unmanned plane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711286747.8A CN107765189A (en) | 2017-12-07 | 2017-12-07 | The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711286747.8A CN107765189A (en) | 2017-12-07 | 2017-12-07 | The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107765189A true CN107765189A (en) | 2018-03-06 |
Family
ID=61277423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711286747.8A Pending CN107765189A (en) | 2017-12-07 | 2017-12-07 | The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107765189A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2816830Y (en) * | 2005-06-17 | 2006-09-13 | 扬州恒信仪表有限公司 | Battery-discharge cure automatic recording instrument |
CN101975927A (en) * | 2010-08-27 | 2011-02-16 | 华南师范大学 | Method and system for estimating remaining available capacity of lithium ion power battery pack |
CN103051005A (en) * | 2011-10-12 | 2013-04-17 | 亚旭电子科技(江苏)有限公司 | Battery charging and discharging management system and method |
CN204203433U (en) * | 2014-09-29 | 2015-03-11 | 天津全华时代航天科技发展有限公司 | Charging and discharging lithium battery registering instrument |
CN104749528A (en) * | 2015-03-30 | 2015-07-01 | 普天新能源车辆技术有限公司 | Power lithium battery capacity determination method |
-
2017
- 2017-12-07 CN CN201711286747.8A patent/CN107765189A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2816830Y (en) * | 2005-06-17 | 2006-09-13 | 扬州恒信仪表有限公司 | Battery-discharge cure automatic recording instrument |
CN101975927A (en) * | 2010-08-27 | 2011-02-16 | 华南师范大学 | Method and system for estimating remaining available capacity of lithium ion power battery pack |
CN103051005A (en) * | 2011-10-12 | 2013-04-17 | 亚旭电子科技(江苏)有限公司 | Battery charging and discharging management system and method |
CN204203433U (en) * | 2014-09-29 | 2015-03-11 | 天津全华时代航天科技发展有限公司 | Charging and discharging lithium battery registering instrument |
CN104749528A (en) * | 2015-03-30 | 2015-07-01 | 普天新能源车辆技术有限公司 | Power lithium battery capacity determination method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20200277080A1 (en) | Systems and methods for in-flight operational assessment | |
US20210070457A1 (en) | Methods and systems for altering power during flight | |
CN107085187A (en) | Echelon utilizes the determination method and device of battery energy storage system consistency maintenance index | |
Bauersfeld et al. | Range, endurance, and optimal speed estimates for multicopters | |
CN206125464U (en) | Many screw parameter testing device for rotor unmanned aerial vehicle | |
CN106542102A (en) | A kind of unmanned plane power-supply management system and its control method | |
WO2017185363A1 (en) | Method, apparatus, and system for controlling unmanned aerial vehicle | |
CN105959181A (en) | System and method for inspecting and detection power inspection unmanned aerial vehicle | |
CN210347811U (en) | New forms of energy car machine integration test system that charges | |
CN208461479U (en) | The battery management system of high-power high voltage battery pack | |
CN206930763U (en) | A kind of lithium battery parameter acquisition system | |
CN107247236A (en) | A kind of lithium battery parameter acquisition system and method | |
CN109725214A (en) | A kind of energy-accumulating power station primary frequency modulation Online Transaction Processing and method | |
CN110015149A (en) | A kind of unmanned plane battery management method and system | |
CN204131181U (en) | A kind of based on the modular battery management system of local with the two-layer management system of the overall situation | |
CN106992573A (en) | Multi-rotor unmanned aerial vehicle charging system and method | |
CN105501455B (en) | A kind of unmanned aerial vehicle comprehensive power integrated system and method | |
CN103023075A (en) | Charging and discharging control method of battery, and electronic device | |
CN207528882U (en) | A kind of small drone electromechanical testing platform | |
CN107765189A (en) | The detection record of charging system and method for multi-rotor unmanned aerial vehicle lithium battery capacity | |
CN207611129U (en) | Battery pack tests system | |
CN106384436A (en) | Intelligent charging system and intelligent charging method | |
CN211148867U (en) | Battery pack diagnostic device for electric vehicle | |
CN207198257U (en) | A kind of DC charging machine detecting device and DC charging motor detecting system | |
WO2020181658A1 (en) | Electric vehicle direct-current charging detection device and method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | 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 |
Application publication date: 20180306 |
|
RJ01 | Rejection of invention patent application after publication |