CN106992587A - A kind of unmanned plane maintaining-managing system - Google Patents
A kind of unmanned plane maintaining-managing system Download PDFInfo
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- CN106992587A CN106992587A CN201710262238.5A CN201710262238A CN106992587A CN 106992587 A CN106992587 A CN 106992587A CN 201710262238 A CN201710262238 A CN 201710262238A CN 106992587 A CN106992587 A CN 106992587A
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- unmanned plane
- solar cell
- power supply
- lithium battery
- cell module
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
- H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
- H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
- H02J9/061—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems for DC powered loads
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/70—Hybrid systems, e.g. uninterruptible or back-up power supplies integrating renewable energies
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of unmanned plane maintaining-managing system, including energy management system, for intelligent power supply；Identification module, the user profile for gathering client's IC-card；System control module, for collecting the user profile collected, the id number of client's IC-card is matched with the unique identification id number that system control module is stored；If the match is successful, system control module sends unlocking command to control module is performed；Control module is performed, the unblock to unmanned plane autopilot is performed for the unlocking command sent according to system controller and action of locking.The present invention is solved lacks a kind of safety management that can either facilitate unmanned plane owner to unmanned plane at present, unmanned plane user is obtained the currently used state of display or/and alarm prompting unmanned plane constantly, the technical problem of unmanned plane efficiency of energy utilization can be improved again.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to unmanned machine management system.
Background technology
With the increasingly maturation of civilian unmanned air vehicle technique, the application of unmanned plane is more and more extensive, and video display are taken photo by plane, land surveying
With true power, geological prospecting, fire-fighting and rescue, security protection inspection and agricultural plant protection etc., the thing followed is asked using, management, safely etc.
Topic continuously emerges.
Unmanned plane on the market is all a kind of open operator scheme at present, can be real using remote control or earth station
Now to the operation of unmanned plane, do not have other Safety Management Measures to unmanned plane in itself.First, client is caused to being bought
Unmanned plane safety management brings many constant, it is impossible to can conveniently be managed as long as holding key as automobile, while so that not having a lot
There are the personnel by system training also arbitrarily to be operated to unmanned plane, hidden danger is brought to autre vie property safety.Secondly,
It is difficult the use for giving for change and preventing other people to unmanned plane that unmanned plane does not have after identity binding, loss with its holder.Finally,
The current state of this equipment of user can not be shown or pointed out on unmanned plane, cause operator to control unmanned plane well
State so that there is very big potential safety hazard in the unmanned plane of airflight.
Moreover, with the development of unmanned air vehicle technique, unmanned plane is in fields such as military affairs, industry, agricultural, traffic, security protections
Greatly developed.But current unmanned plane is substantially used as fuel using lithium battery, battery, fuel cell etc..It is limited to nobody
The design size of machine, the energy entrained by unmanned plane is limited, and which limits the airborne period of unmanned plane, voyage etc., shadow
Ring the limited load of unmanned plane and mission requirements.Solar energy is as a kind of brand-new energy, and its cleanliness without any pollution, source are never withered
Exhaust, the features such as maintenance measure is simple, it is increasingly received significant attention, this has also promoted solar energy unmanned plane to produce and send out
Exhibition.Solar energy unmanned plane as following unmanned plane developing direction, if merely using solar energy energy supply, can be by illumination, outer
Boundary's environment etc. influences, and can reduce the adaptability of solar energy unmanned plane.
The content of the invention
It is an object of the invention to：A kind of unmanned plane maintaining-managing system is provided, with solve at present lack one kind can either
Facilitate safety management of the unmanned plane owner to unmanned plane, unmanned plane user is obtained display or/and alarm constantly
Device reminds the currently used state of unmanned plane, can improve the technical problem of unmanned plane efficiency of energy utilization again.
The technical solution adopted by the present invention is as follows：
A kind of unmanned plane maintaining-managing system, including
Energy management system, for intelligent power supply；
Identification module, the user profile for gathering client's IC-card；
System control module, for collecting the user profile collected, the id number of client's IC-card and system are controlled
The unique identification id number of module storage is matched；If the match is successful, system control module is sent to control module is performed
Unlocking command；
Control module is performed, the solution to unmanned plane autopilot is performed for the unlocking command sent according to system controller
Lock and action of locking.
Further, energy management system includes energy management controller and lithium battery pack, energy management controller electricity
It is connected with battery status detection module, intelligent recharge and discharge module and is electrically connected to the unmanned plane power supply unit of airborne control end；Lithium
Battery component is electrically connected with lithium battery protection circuit, and by lithium battery protection circuit be electrically connected to battery status detection module and
Intelligent recharge and discharge module.
Further, in addition to the solar cell module, DC-DC converter and the maximal power tracing mould that are sequentially connected
Block, maximal power tracing module is electrically connected to energy management controller；Solar cell module and the DC-DC conversion being sequentially connected
Device is also electrically connected with battery status detection module；Solar cell module is to lithium battery pack charge mode, solar battery group
Part is directly to unmanned plane power supply unit powering mode, solar cell module simultaneously to lithium battery pack and unmanned plane power supply unit
Powering mode, solar cell module and lithium battery pack combine to unmanned plane power supply unit powering mode, lithium battery pack to
Unmanned plane power supply unit powering mode.
Further, the selection flow of energy management system comprises the following steps：
(1) according to unmanned plane power supply unit power supply state, judge whether unmanned plane power supply unit runs, if unmanned plane is powered
Unit is run, then performs step 2；If unmanned plane power supply unit is not run, step 3 is performed；
(2) according to solar cell module output state, judge whether solar cell module has power output, if the sun
Energy battery component has power output, then performs step 4；If solar cell module does not have power output, step 5 is performed；
(3) according to lithium battery pack state of charge, whether be full, if lithium battery pack electricity if judging lithium battery pack electricity
It is full, then unmanned plane energy management system performs holding state；If lithium battery pack electricity is discontented with, step 6 is performed；
(4) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell is judged
Whether component power output, which meets unmanned plane power supply unit, is normally run, if solar cell module power output meets unmanned plane
Power supply unit is normally run, then performs step 7；If solar cell module power output can not meet unmanned plane power supply unit just
Often operation, then perform solar cell module and lithium battery pack combined to unmanned plane power supply unit powering mode；
(5) according to lithium battery pack state of charge, judge whether lithium battery pack electricity is less than warning value, if lithium battery group
Part electricity is less than warning value, and alarming and starting landing prepares；If lithium battery pack electricity is not below warning value, lithium electricity is performed
Pond component is to unmanned plane power supply unit powering mode；
(6) according to solar cell module output state, judge whether solar cell module has power output, if the sun
Energy battery component has power output, then performs solar cell module to lithium battery pack charge mode；If solar battery group
Part does not have power output, then unmanned plane energy management system performs holding state；
(7) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell is judged
Whether component power output has surplus, if solar cell module power output has surplus, performs solar cell module simultaneously
To lithium battery pack and unmanned plane power supply unit powering mode；If solar cell module power output does not have surplus, perform
Solar cell module is directly to unmanned plane power supply unit powering mode.
In summary, by adopting the above-described technical solution, the beneficial effects of the invention are as follows：
The energy management system that the present invention is provided as unmanned plane energy resource system control and regulation center, it is possible to achieve the sun
Energy battery component and lithium battery pack are common to unmanned plane energy supply, it is possible to achieve solar module power output is adjusted, to lithium
Battery component carries out intelligent management.In the case where solar cell module power output is sufficient, more lithium electricity are retained as far as possible
The energy of pond component；In the case where solar cell module power output is not enough, then supplemented by lithium battery pack.This hair
It is bright to have also been devised complete unmanned plane energy control flow, it is ensured that energy control system in varied situations, can be
Unmanned plane provides stable, sufficient energy, with reference to the advantage of solar cell and lithium battery, and rationally control and distribution energy make
With the utilization rate of the raising unmanned plane energy, so as to realize the long boat flight of unmanned plane；Meanwhile, the present invention can be maximally utilized
Energy produced by solar cell module, increases the voyage of unmanned plane.The present invention, which also has, to be easily achieved, using convenient etc. excellent
Point；This invention also solves this open-sky technique and problem of management of unmanned plane, unmanned plane owner is facilitated to unmanned plane
Safety management, it is to avoid other staff's arbitrarily operates with, the protection unmanned plane owner and autre vie property safety；Together
When by way of display or alarm the moment remind currently used state of the unmanned plane user on unmanned plane, if any
Problem carries out maintenance in time, greatly the potential safety hazard of reduction unmanned plane.
Brief description of the drawings
Fig. 1 is overall system architecture schematic diagram；
Fig. 2 is the structural relation schematic diagram of unmanned plane maintaining-managing system and energy management system；
Fig. 3 is energy management system control model selection flow chart.
Embodiment
All features disclosed in this specification, can be with any in addition to mutually exclusive feature and/or step
Mode is combined.
With reference to Fig. 1~3 pair, the present invention elaborates.
A kind of unmanned plane maintaining-managing system, including
Energy management system, for intelligent power supply；
Identification module, the user profile for gathering client's IC-card；
System control module, IC-card and IC-card RF detection module of the identification module connection with read-write capability,
For collecting the user profile collected, the unique identification ID that the id number of client's IC-card and system control module are stored
Code is matched；If the match is successful, system control module sends unlocking command to control module is performed；
Control module is performed, the solution to unmanned plane autopilot is performed for the unlocking command sent according to system controller
Lock and action of locking.
To save electric power, (ID values are matched, unmanned plane state is normal, held after the completion of unmanned plane maintaining-managing system task
Row control module unlocks autopilot), it will enter resting state：Display output and backlight are closed, transmission makes identification
Module enters the order of energy-saving mode, while cut-out and alarm and the communication link of execution control module, with this so that whole
Unmanned plane maintaining-managing system is in a kind of low-power consumption mode, reduces the kwh loss to unmanned plane.
The display that the present invention is used shows the title and purposes of this equipment first, then shows that identification module is detected
The ID values of the correct IC-card arrived, then will show the behaviour in service of this TV station unmanned plane, to prompt the user whether to need to be serviced
Maintenance, the character of last display reminding.
The control command that alarm can be sent according to system control module sends different prompting warning sound：Correctly carry
Show sound, maintaining prompt tone, IC-card false alarm sound.
Energy management system include solar cell module, DC-DC converter, lithium battery pack, lithium battery protection circuit,
Energy management controller, system control module, unmanned plane power supply unit, energy management controller include energy management controller,
Battery status detection module, intelligent recharge and discharge module, maximal power tracing module；Solar cell module and DC-DC converter
It is connected, DC-DC converter is connected with maximal power tracing module and battery status detection module respectively, lithium battery pack and lithium electricity
Pond protection circuit is connected, and lithium battery protection circuit is connected with intelligent recharge and discharge module and battery status detection module respectively, the energy
Management Controller controls mould with battery status detection module, intelligent recharge and discharge module, maximal power tracing module, system respectively
Block, unmanned plane power supply unit are connected, and system control module is connected with unmanned plane power supply unit.
The solar cell module is generally flexible thin-film solar piece, can be rationally laid on according to the type of unmanned plane
The places such as wing, the fuselage of unmanned plane；The lithium battery pack is the energy-storage travelling wave tube of unmanned plane, and its energy density should meet nobody
The task of machine needs；The maximal power tracing module can make solar cell module with maximum power output, can improve the sun
The utilization ratio of energy battery component；The intelligent recharge and discharge module can be completed according to the instruction of energy management controller to lithium electricity
The charging and discharging task of pond component, can possess the functions such as quick charge, protection lithium battery, safe-discharge；The battery status
Detection module monitors the parameters such as voltage, the electric current of solar cell module and lithium battery pack in real time, accurately, is real-time transmitted to energy
Source control controller；The information of the energy management controller comprehensive energy Management Controller each several part, unmanned plane power supply unit
Operation information and system control module relevant information and instruction, complete to solar cell module and the energy of lithium battery pack
Source control, distribution and utilization, it is ensured that unmanned plane power supply unit is normally run；The system control module controls the power of unmanned plane
System, control system, communication system and other unmanned plane correlation modules, the relevant operational state of unmanned plane is transmitted in real time
Control instruction is delivered into energy management controller to energy management controller, and as needed；The unmanned plane power supply unit bag
Include the power supply unit needed for dynamical system, control system, communication system and other unmanned planes.
Energy management controller receives the information of each several part in energy management system, including solar cell module operation shape
State, lithium battery pack running status, the signal of the operation information of unmanned plane power supply unit and unmanned main control module and refer to
Order, after comprehensive various information, according to predetermined operating mode, completes energy distribution；Wherein, the operation shape of solar cell module
State, can be by the DC-DC converter outputs state detection that is connected with solar cell module, and the running status of lithium battery pack can
Detected in the lithium battery protection circuit being connected with lithium battery pack.
The output energy of solar cell module has two flow directions in the energy management system, and one is to be filled with lithium battery
Component is as energy reserve, and two be to directly feed unmanned plane power supply unit.Energy management controller uses dynamic power supplies path tube
Reason technology (Dynamic Power Path Management, DPPM), the electric energy acquired in solar cell module is being filled with
Lithium battery pack and feed to and carry out dynamic dispatching between unmanned plane power supply unit, to maximally utilize the output work of solar cell
Rate.
Energy management system realizes different energy control patterns under different running statuses, including：Solar battery group
Part is to lithium battery pack charge mode, solar cell module directly to unmanned plane power supply unit powering mode, solar cell
Component simultaneously to lithium battery pack and unmanned plane power supply unit powering mode, solar cell module and lithium battery pack combine to
Unmanned plane power supply unit powering mode, lithium battery pack are to unmanned plane power supply unit powering mode.
The selection judging unit of solar energy unmanned plane energy management system control model includes, and unmanned plane power supply unit is powered
Condition adjudgement unit, solar cell module output state judging unit, lithium battery pack state of charge judging unit；
The selection of the various patterns of solar energy unmanned plane energy management system, it is necessary first to meet the energy of unmanned plane power supply unit
Source is supplied, particularly the safety and steady operation and control system, the stable operation of communication system of unmanned plane dynamical system load；Together
When, the switching of different energy sources control model should meet quick, steady, it is impossible to influence the normal operation of unmanned plane；Difference control mould
The selection of formula should be based on maximally utilizing solar cell power output and the safe and efficient utilization of lithium battery.
When unmanned plane is without operation, i.e., it need not be powered to unmanned plane power supply unit, solar cell module should be right in time
Lithium battery pack charges；When unmanned plane is normally run, when illumination is sufficient, solar cell module power output can meet nothing
In the case of man-machine power supply unit demand, energy directly can be provided to unmanned plane power supply unit, due to solar cell module
Power output and unstable, it is necessary to according to the energy demand of unmanned plane power supply unit, dynamic regulation power output；Unmanned plane is just
Often during operation, when illumination is sufficient, solar cell module power output can meet the feelings of unmanned plane power supply unit energy requirement
Under condition, when the electricity for detecting lithium battery pack is discontented, ensureing unmanned plane power supply unit normally in the case of operation, can be with
By dynamic power supplies path management technology, to charging for lithium battery pack；When unmanned plane is normally run, when illumination is not enough,
Solar cell module power output is when can not fully meet the energy requirement of unmanned plane power supply unit, it is necessary to by lithium battery group
Part supplement output energy, meets unmanned plane power supply unit and normally runs；When unmanned plane is normally run, solar cell module without
During power output, start lithium battery pack and individually unmanned plane power supply unit is powered；When unmanned plane is normally run, lithium battery pack
Individually in the case of power supply, when lithium battery pack electricity is less than default charge value, start alarm.
A kind of solar energy unmanned plane energy management system, the selection flow of control model comprises the following steps：
(1) according to unmanned plane power supply unit power supply state, judge whether unmanned plane power supply unit runs, if unmanned plane is powered
Unit is run, then performs step 2；If unmanned plane power supply unit is not run, step 3 is performed；
(2) according to solar cell module output state, judge whether solar cell module has power output, if the sun
Energy battery component has power output, then performs step 4；If solar cell module does not have power output, step 5 is performed；
(3) according to lithium battery pack state of charge, whether be full, if lithium battery pack electricity if judging lithium battery pack electricity
It is full, then unmanned plane energy management system performs holding state；If lithium battery pack electricity is discontented with, step 6 is performed；
(4) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell is judged
Whether component power output, which meets unmanned plane power supply unit, is normally run, if solar cell module power output meets unmanned plane
Power supply unit is normally run, then performs step 7；If solar cell module power output can not meet unmanned plane power supply unit just
Often operation, then perform solar cell module and lithium battery pack combined to unmanned plane power supply unit powering mode；
(5) according to lithium battery pack state of charge, judge whether lithium battery pack electricity is less than warning value, if lithium battery group
Part electricity is less than warning value, and alarming and starting landing prepares；If lithium battery pack electricity is not below warning value, lithium electricity is performed
Pond component is to unmanned plane power supply unit powering mode；
(6) according to solar cell module output state, judge whether solar cell module has power output, if the sun
Energy battery component has power output, then performs solar cell module to lithium battery pack charge mode；If solar battery group
Part does not have power output, then unmanned plane energy management system performs holding state；
(7) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell is judged
Whether component power output has surplus, if solar cell module power output has surplus, performs solar cell module simultaneously
To lithium battery pack and unmanned plane power supply unit powering mode；If solar cell module power output does not have surplus, perform
Solar cell module is directly to unmanned plane power supply unit powering mode.
There is an IC-card that unique match is recognized therewith in unmanned plane maintaining-managing system, when unmanned plane dispatches from the factory, in IC-card
Will typing this TV station equipment relevant parameter, including the performance of unmanned plane, purposes, access times etc., when equipment is sold, nothing
Man-machine owner's identity will be bound with the IC of unmanned plane.
The management method implemented by said system, including：
1) electric on unmanned plane, the system control module of unmanned plane maintaining-managing system sends control command and controls mould to execution
Block is locked by unmanned plane autopilot；
2) system control module shows the title and purposes of the machine by display, and exports prompting operator's progress identity
The character of identification, alarm carries out alarm；
3) when IC-card enters detection zone, the Card Reader chip of identification module, which reads the content in IC-card and is sent to, is
In control module of uniting；
4) the unique identification id number progress that system control module stores the id number of IC-card and system control module
Match somebody with somebody：If correct id number will be sent to display and be shown, sent by both id number matchings, system control module simultaneously
Correct alarm command is correct to alarm prompting ID；If both mismatch, system control module will send the warning of error ID
Information is shown to display, sends alarm command to alarm, while sending locked control command to execution control module
Locked unmanned plane autopilot, afterwards system control module will continue waiting for identification module and send new information；
5) system control module changes storage value and is sent to identification region by communication interface, will be amended interior
Hold in write-in IC-card.
What the present invention was not elaborated partly belongs to techniques well known, and those skilled in the art are according to existing description
It can on the premise of not paying creative work be implemented, therefore, be repeated no more.
Claims (4)
1. a kind of unmanned plane maintaining-managing system, it is characterised in that including
Energy management system, for intelligent power supply；
Identification module, the user profile for gathering client's IC-card；
System control module, for collecting the user profile collected, by the id number and system control module of client's IC-card
The unique identification id number of storage is matched；If the match is successful, system control module sends unblock to control module is performed
Order；
Perform control module, performed for the unlocking command sent according to system controller the unblock to unmanned plane autopilot with
Lock action.
2. a kind of unmanned plane maintaining-managing system as claimed in claim 1, it is characterised in that energy management system includes the energy
Management Controller and lithium battery pack, energy management controller are electrically connected with battery status detection module, intelligent recharge and discharge module
With the unmanned plane power supply unit for being electrically connected to airborne control end；Lithium battery pack is electrically connected with lithium battery protection circuit, and passes through
Lithium battery protection circuit is electrically connected to battery status detection module and intelligent recharge and discharge module.
3. a kind of unmanned plane management platform as claimed in claim 2, it is characterised in that the also solar-electricity including being sequentially connected
Pond component, DC-DC converter and maximal power tracing module, maximal power tracing module are electrically connected to energy management controller；
The solar cell module and DC-DC converter being sequentially connected also are electrically connected with battery status detection module；Solar battery group
Part is to lithium battery pack charge mode, solar cell module directly to unmanned plane power supply unit powering mode, solar cell
Component simultaneously to lithium battery pack and unmanned plane power supply unit powering mode, solar cell module and lithium battery pack combine to
Unmanned plane power supply unit powering mode, lithium battery pack are to unmanned plane power supply unit powering mode.
4. a kind of unmanned plane management platform as claimed in claim 3, it is characterised in that the selection flow bag of energy management system
Include following steps：
(1) according to unmanned plane power supply unit power supply state, judge whether unmanned plane power supply unit runs, if unmanned plane power supply unit
Operation, then perform step 2；If unmanned plane power supply unit is not run, step 3 is performed；
(2) according to solar cell module output state, judge whether solar cell module has power output, if solar-electricity
Pond component has power output, then performs step 4；If solar cell module does not have power output, step 5 is performed；
(3) according to lithium battery pack state of charge, whether be full, if lithium battery pack electricity is if judging lithium battery pack electricity
Full, then unmanned plane energy management system performs holding state；If lithium battery pack electricity is discontented with, step 6 is performed；
(4) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell module is judged
Whether power output, which meets unmanned plane power supply unit, is normally run, and is powered if solar cell module power output meets unmanned plane
Unit is normally run, then performs step 7；If solar cell module power output can not meet unmanned plane power supply unit and normally transport
OK, then perform solar cell module and lithium battery pack is combined to unmanned plane power supply unit powering mode；
(5) according to lithium battery pack state of charge, judge whether lithium battery pack electricity is less than warning value, if lithium battery pack is electric
Amount is less than warning value, and alarming and starting landing prepares；If lithium battery pack electricity is not below warning value, lithium battery group is performed
Part is to unmanned plane power supply unit powering mode；
(6) according to solar cell module output state, judge whether solar cell module has power output, if solar-electricity
Pond component has power output, then performs solar cell module to lithium battery pack charge mode；If solar cell module does not have
There is power output, then unmanned plane energy management system performs holding state；
(7) according to unmanned plane power supply unit power supply state and solar cell module output state, solar cell module is judged
Whether power output has surplus, if solar cell module power output has surplus, performs solar cell module simultaneously to lithium
Battery component and unmanned plane power supply unit powering mode；If solar cell module power output does not have surplus, the sun is performed
Energy battery component is directly to unmanned plane power supply unit powering mode.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107856860A (en) * | 2017-11-30 | 2018-03-30 | 徐朋 | A kind of solar energy plant protection unmanned plane |
| CN109774951A (en) * | 2019-03-13 | 2019-05-21 | 江苏科技大学 | A kind of energy autonomous management system for the amphibious aircraft of air-sea |
| WO2020147118A1 (en) * | 2019-01-18 | 2020-07-23 | 深圳市大疆创新科技有限公司 | Power management method and device and mobile robot |
| WO2021078163A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method, apparatus and device, and storage medium |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
| WO2015196127A1 (en) * | 2014-06-20 | 2015-12-23 | Colorado Seminary, Which Owns And Operates The University Of Denver | Mobile self-leveling landing platform for uavs |
| CN105539869A (en) * | 2016-02-03 | 2016-05-04 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintenance and management system and method |
| CN105905305A (en) * | 2016-04-22 | 2016-08-31 | 中国计量大学 | Energy management system of solar unmanned aerial vehicle |
-
2017
- 2017-04-20 CN CN201710262238.5A patent/CN106992587A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
| WO2015196127A1 (en) * | 2014-06-20 | 2015-12-23 | Colorado Seminary, Which Owns And Operates The University Of Denver | Mobile self-leveling landing platform for uavs |
| CN105539869A (en) * | 2016-02-03 | 2016-05-04 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintenance and management system and method |
| CN105905305A (en) * | 2016-04-22 | 2016-08-31 | 中国计量大学 | Energy management system of solar unmanned aerial vehicle |
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| CN107856860A (en) * | 2017-11-30 | 2018-03-30 | 徐朋 | A kind of solar energy plant protection unmanned plane |
| WO2020147118A1 (en) * | 2019-01-18 | 2020-07-23 | 深圳市大疆创新科技有限公司 | Power management method and device and mobile robot |
| CN109774951A (en) * | 2019-03-13 | 2019-05-21 | 江苏科技大学 | A kind of energy autonomous management system for the amphibious aircraft of air-sea |
| WO2021078163A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method, apparatus and device, and storage medium |
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