CN106998095A - A kind of unmanned plane management platform - Google Patents
A kind of unmanned plane management platform Download PDFInfo
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- CN106998095A CN106998095A CN201710262239.XA CN201710262239A CN106998095A CN 106998095 A CN106998095 A CN 106998095A CN 201710262239 A CN201710262239 A CN 201710262239A CN 106998095 A CN106998095 A CN 106998095A
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- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 90
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 90
- 238000001514 detection method Methods 0.000 claims abstract description 19
- 238000012544 monitoring process Methods 0.000 claims abstract description 15
- 230000004224 protection Effects 0.000 claims abstract description 13
- 210000004027 cell Anatomy 0.000 claims description 86
- 230000005611 electricity Effects 0.000 claims description 26
- 238000004891 communication Methods 0.000 claims description 14
- 238000005516 engineering process Methods 0.000 claims description 6
- 210000003850 cellular structure Anatomy 0.000 claims description 2
- 238000010977 unit operation Methods 0.000 claims description 2
- 238000000465 moulding Methods 0.000 claims 2
- 238000007726 management method Methods 0.000 description 48
- 238000000034 method Methods 0.000 description 5
- 238000005286 illumination Methods 0.000 description 4
- 206010038743 Restlessness Diseases 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005183 dynamical system Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- XGCDBGRZEKYHNV-UHFFFAOYSA-N 1,1-bis(diphenylphosphino)methane Chemical compound C=1C=CC=CC=1P(C=1C=CC=CC=1)CP(C=1C=CC=CC=1)C1=CC=CC=C1 XGCDBGRZEKYHNV-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
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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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- 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
- H02J7/0068—Battery or charger load switching, e.g. concurrent charging and load supply
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- 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
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/56—Power conversion systems, e.g. maximum power point trackers
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of unmanned plane management platform, including airborne control end and remote monitoring and control end, airborne control end is connected with the control of unmanned plane autopilot and realizes the control to unmanned plane structure platform, and the power supply of airborne control end carries out intelligent control by energy management system；Energy management system includes energy management controller, lithium battery pack and solar cell module, and energy management controller is electrically connected with battery status detection module, intelligent recharge and discharge module and maximal power tracing module；Lithium battery pack is electrically connected with lithium battery protection circuit, and is electrically connected to battery status detection module and intelligent recharge and discharge module by lithium battery protection circuit；Solar cell module is electrically connected with DC DC converters, and is electrically connected by DC DC converters in battery status detection module and maximal power tracing module.The present invention is solved to be lacked one kind and can either improve unmanned plane efficiency of energy utilization at present, can also strengthen the technical problem of the management platform of unmanned plane management and control.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to a kind of unmanned plane management platform.
Background technology
According to《Civilian push-button aircraft system driver management temporary provisions》, in isolation spatial domain over the horizon operation
Unmanned plane needs accredited flight, according to air traffic control policy, and the kilometer range of airport overhead 8 is interior and PLA Air Force sets
Vertical forbidden zone and other Temporary Restricted Areas can not all enter flight.But the domestic supervisory system to low latitude SUAV is still at present
Imperfection, and unmanned machine equipment design reasons itself, management can not be monitored to unmanned operators by causing so that nobody
The winged phenomenon of the black winged unrest of machine is commonplace, while the airmanship of pilot is uneven, causes the unmanned plane of airflight to be deposited
In very big potential safety hazard.So the supervision to unmanned plane needs great raising, the not exclusively safety of manufacturer at present
Training is strengthened, at the same with greater need for the management and control for being the supervision to client unmanned plane and control, strengthening unmanned plane during flying region.
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 management platform is provided, to solve to lack one kind at present and can either improve
Unmanned plane efficiency of energy utilization, can also strengthen the technical problem of the management platform of unmanned plane management and control.
The technical solution adopted by the present invention is as follows：
A kind of unmanned plane management platform, including the airborne control end in body and remote monitoring and the control on ground
End, airborne control end is connected with the control of unmanned plane autopilot and realizes the control to unmanned plane structure platform, airborne control end
Power supply carries out intelligent control by energy management system.
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.
Further, airborne control end also includes system control module, and system control module is electrically connected with identification mould
Block, alignment system, display, alarm, execution control module and wireless telecommunication system；System control module is by performing control
Module unmanned plane autopilot is communicated to connect, and system control module passes through wireless telecommunication system and remote monitoring and control end communication link
Connect.
Further, remote monitoring includes the webserver with wireless telecommunication system communication connection with control end, internal
Provided with the Surveillance center that row information is exchanged is entered with the webserver, the Orientation on map of Surveillance center's connection displaing coordinate shows mould
The remote control module of block, the alarm module for prompting and unauthorized operation UAS.
Further, identification module is provided with the IC-card RF Technology for Measuring with read-write capability.
In summary, by adopting the above-described technical solution, the beneficial effects of the invention are as follows：
1. the energy management system that the present invention is provided is used as the control and regulation center of unmanned plane energy resource system, it is possible to achieve too
Positive energy battery component and lithium battery pack are common to be energized to unmanned plane, it is possible to achieve solar module power output is adjusted, right
Lithium battery pack carries out intelligent management.In the case where solar cell module power output is sufficient, more lithiums are retained as far as possible
The energy of battery component；In the case where solar cell module power output is not enough, then supplemented by lithium battery pack.This
Invention have also been devised complete unmanned plane energy control flow, it is ensured that energy control system in varied situations, can be with
Stable, sufficient energy is provided for unmanned plane, with reference to the advantage of solar cell and lithium battery, 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.
2. using after such scheme, operator's identity could unlock unmanned plane autopilot after being matched with unmanned plane, by fixed
Position system carries out position positioning to unmanned plane, and will be sent to Surveillance center for information about by wireless communication module, passes through prison
Control center carries out remote monitoring and control to unmanned plane, solves the potential safety hazard that the current black winged unrest of unmanned plane flies to bring, reinforcement pair
The security monitoring and management in aerial region, reduce the potential safety hazard of unmanned plane, protection the people's lives and property safety.Surveillance center
To unmanned plane during flying, the record using process and prompting, facilitate safety management and maintaining of the client to unmanned machine equipment.
Brief description of the drawings
Fig. 1 is overall system architecture schematic diagram；
Fig. 2 is the structural relation schematic diagram of airborne control end 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 management platform, including the airborne control end in body and remote monitoring and the control on ground
End, airborne control end is connected with the control of unmanned plane autopilot and realizes the control to unmanned plane structure platform, airborne control end
Power supply carries out intelligent control by energy management system.
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.
And the identification module and alignment system in above-mentioned airborne control end are connected with system control module, identity is tested
Card information and geographical location information are delivered to system control module and judged, system control module is passed by wireless telecommunication system
Defeated signal is to remote monitoring and control end, the display and alarm that the judged result of remote monitoring and control end is passed through into connection
Reminded, and send a command to execution control module, performed control module and be connected with unmanned plane autopilot.
For the ease of read-write data, identification module is provided with the IC-card RF Technology for Measuring of read-write capability.
Remote monitoring includes the webserver communicated with airborne control end with control end, and inside is provided with and the webserver
Enter the Surveillance center of row information exchange, the Orientation on map display module of Surveillance center's connection displaing coordinate, the alarm for prompting
The remote control module of reminding module and unauthorized operation UAS, Surveillance center is sent instructions in airborne control end
System control module.
The management method implemented using said system is comprised the following steps：
1. electric on unmanned plane, the system control module of airborne control end sends order of locking to control module is performed, by nothing
Man-machine autopilot is locked so that unmanned controller or earth station can not manipulate to it；
2. display shows that the title, purposes and prompting user of unmanned plane carry out the prompting character of identification, system
The prompt command that control module sends progress identification carries out auditory tone cues to alarm；
3. the system control module moment inquire about identification module detection information, while processing by alignment system transmission Lai
Location data；
4. system control module sends the id number and location information of this equipment unmanned plane by wireless communication module
To Surveillance center；
5. unmanned plane is checked for information about first by Surveillance center, while judging whether unmanned plane is according to location data
Legal flight range, the control command of Surveillance center's passback afterwards is to system control module；
Unmanned plane autopilot is unlocked to control module is performed 6. system control module sends unlocking command.
In above-mentioned identification, the IC-card radio frequency detection zone moment of identification module sends detection signal and carries out IC-card
Detection, if detect IC-card, Card Reader chip will read out the content in IC-card, and by communication interface by IC-card
Content is sent in system control module.System control module is obtained after IC-card content, first, the id number and system of IC-card
The unique identification id number of control module storage is matched, if both mismatch, system control module will send mistake
ID warning message is shown to display, alarm command is sent to alarm, while unmanned plane autopilot will be unable to unblock.
If it does, display is correctly shown, alarm sends correct prompt tone, and simultaneity factor control module parses the interior of IC-card
Hold, show the currently used state of unmanned plane, while change storage value and identification region is sent to by communication interface, will
In amended content write-in IC-card.System control module sends unlocking command and unmanned plane autopilot is entered to control module is performed
Row unblock.
Monitoring in real time
1. alignment system, which is proceeded by, searches star positioning, alignment system periodically passes through location data after positioning successfully
Communication interface sends system control module to, and system control module parses the location information of unmanned plane, by the position coordinates of positioning,
Height above sea level, movement velocity and time etc. and status information and the id number packing of unmanned plane are sent out by wireless communication module
See off.
2. the webserver is received after the information that unmanned aerial vehicle onboard control end is sent by wireless communication module, it will receive
Information transmission to Surveillance center.
3. Surveillance center is obtained after data, the id number of unmanned plane is parsed first, and having for unmanned plane is inquired about according to id number
Close information：Subscriber data, the type of unmanned plane, use condition, state of purposes and unmanned machine equipment etc..Secondly nothing is parsed
Man-machine position coordinates, and electronic map progress position display is imported, while passing through the operation area that position coordinates differentiates unmanned plane
Whether domain is legal, if unmanned plane is shown normally in legal area monitoring picture, and otherwise warning prompt module sends prompting police
Accuse, remind Surveillance center to be controlled operation.Again, Surveillance center's moment monitors the flight attitude data of unmanned plane, judges nothing
Man-machine whether to fly into no-fly zone, whether flying height, which exceedes limitation, requires whether flying speed exceeds the speed limit, if criminal manipulation
Surveillance center can be sent to unmanned plane by remote control module and be ordered：1st, prompting alarm command can be sent to airborne control
End, unmanned operators are pointed out by display and alarm, unmanned plane is in illegal region, more than flying height limitation and
Hypervelocity etc..2nd, the manipulation power that control command deprives unmanned plane is sent, if the warning that unmanned operators ignore control centre is carried
Show, control centre can deprive the control of unmanned note by force by remote control module so that the unmanned plane on ground
It can not start, be maked a return voyage automatically landing in unmanned plane in-flight.
Finally, as the usage record that unmanned note is store in the IC-card of identification, unmanned plane is carrying out identification
When, the content for the related unmanned plane maintaining being stored in IC-card is shown the display by airborne control end, together
When use process of the ground monitoring center also to unmanned plane backed up and recorded, pass through the use that Surveillance center shows unmanned plane
State, Surveillance center can remind client to carry out corresponding maintenance to unmanned plane according to Contents for Monitoring.
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 (7)
1. a kind of unmanned plane management platform, it is characterised in that including the airborne control end and the long-range prison on ground in body
Control and control end, airborne control end are connected with the control of unmanned plane autopilot and realize the control to unmanned plane structure platform, airborne
The power supply of control end carries out intelligent control by energy management system.
2. a kind of unmanned plane management platform as claimed in claim 1, it is characterised in that energy management system includes energy management
Controller and lithium battery pack, energy management controller are electrically connected with battery status detection module, intelligent recharge and discharge module and electricity
It is connected to the unmanned plane power supply unit of airborne control end；Lithium battery pack is electrically connected with lithium battery protection circuit, and passes through lithium electricity
Pond 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.
5. a kind of unmanned plane management platform as described in any one of Claims 1 to 4, it is characterised in that airborne control end is also wrapped
Include system control module, system control module is electrically connected with identification module, alignment system, display, alarm, performs control
Molding block and wireless telecommunication system；System control module is communicated to connect by performing control module unmanned plane autopilot, system control
Molding block is communicated to connect by wireless telecommunication system and remote monitoring with control end.
6. a kind of unmanned plane management platform as claimed in claim 5, it is characterised in that remote monitoring includes and nothing with control end
Supervised provided with the Surveillance center that row information is exchanged is entered with the webserver webserver of line communication system communication connection, inside
Control center connects Orientation on map display module, the alarm module for prompting and the unauthorized operation unmanned plane system of displaing coordinate
The remote control module of system.
7. a kind of unmanned plane management platform as claimed in claim 5, it is characterised in that identification module, which is provided with, has read-write
The IC-card RF Technology for Measuring of function.
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| CN201710262239.XA CN106998095A (en) | 2017-04-20 | 2017-04-20 | A kind of unmanned plane management platform |
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| CN107551569A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of study course aircraft with solar panel |
| CN107554800A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of aircraft with solar panel |
| CN107554769A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of anti-lost aircraft with solar panel |
| CN107831783A (en) * | 2017-11-10 | 2018-03-23 | 南昌航空大学 | A kind of ground station control system for supporting multiple no-manned plane autonomous flight |
| CN107831786A (en) * | 2017-11-14 | 2018-03-23 | 廊坊市伟东电气设备有限公司 | A kind of cruise unmanned plane continuation of the journey control system based on battery energy storage system |
| CN108196569A (en) * | 2017-12-20 | 2018-06-22 | 中国航天空气动力技术研究院 | A kind of general unmanned machine earth station |
| CN108762311A (en) * | 2018-06-22 | 2018-11-06 | 东汉太阳能无人机技术有限公司 | The flight control method and device of aircraft |
| CN110884311A (en) * | 2019-12-19 | 2020-03-17 | 酷黑科技（北京）有限公司 | Power supply control system and three-dimensional traffic operation system of hovercar |
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| CN107551569A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of study course aircraft with solar panel |
| CN107554800A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of aircraft with solar panel |
| CN107554769A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of anti-lost aircraft with solar panel |
| CN107831783A (en) * | 2017-11-10 | 2018-03-23 | 南昌航空大学 | A kind of ground station control system for supporting multiple no-manned plane autonomous flight |
| CN107831786A (en) * | 2017-11-14 | 2018-03-23 | 廊坊市伟东电气设备有限公司 | A kind of cruise unmanned plane continuation of the journey control system based on battery energy storage system |
| CN108196569A (en) * | 2017-12-20 | 2018-06-22 | 中国航天空气动力技术研究院 | A kind of general unmanned machine earth station |
| CN108196569B (en) * | 2017-12-20 | 2021-02-09 | 中国航天空气动力技术研究院 | General unmanned aerial vehicle ground satellite station |
| CN108762311A (en) * | 2018-06-22 | 2018-11-06 | 东汉太阳能无人机技术有限公司 | The flight control method and device of aircraft |
| CN110884311A (en) * | 2019-12-19 | 2020-03-17 | 酷黑科技（北京）有限公司 | Power supply control system and three-dimensional traffic operation system of hovercar |
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Application publication date: 20170801 |