CN110065645A - High-precision UAV Flight Control System - Google Patents
High-precision UAV Flight Control System Download PDFInfo
- Publication number
- CN110065645A CN110065645A CN201910331292.XA CN201910331292A CN110065645A CN 110065645 A CN110065645 A CN 110065645A CN 201910331292 A CN201910331292 A CN 201910331292A CN 110065645 A CN110065645 A CN 110065645A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- grid
- landing platform
- precision
- flight control
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- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
- Y02T90/167—Systems integrating technologies related to power network operation and communication or information technologies for supporting the interoperability of electric or hybrid vehicles, i.e. smartgrids as interface for battery charging of electric vehicles [EV] or hybrid vehicles [HEV]
-
- 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
- Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
- Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
- Y04S30/00—Systems supporting specific end-user applications in the sector of transportation
- Y04S30/10—Systems supporting the interoperability of electric or hybrid vehicles
- Y04S30/12—Remote or cooperative charging
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention relates to unmanned plane charging technique fields, specifically high-precision UAV Flight Control System, for solving the problem of that existing unmanned plane midway cannot charge and result in unmanned plane inspection radius and be restricted.The present invention includes charging base station system and fuselage docking system, and the charging base station system includes matrix landing platform, and multiple grids are equipped on the matrix landing platform, are connected with charge power supply in each grid；The fuselage docking system includes the multiple ventral contacts that is mounted on body bottom surface and can dock with grid.By establishing matrix landing platform in position in the present invention, when unmanned plane does not have electricity fastly, it can be dropped on matrix landing platform and be charged by remote control unmanned plane, unmanned plane just no longer needs to charging of making a return voyage in this way, so that the inspection radius of unmanned plane is bigger, travelable voyage is farther.
Description
Technical field
The present invention relates to unmanned plane charging technique fields, more particularly to high-precision UAV Flight Control System.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, Huo Zheyou
Car-mounted computer fully or intermittently automatically operates, unmanned plane press application field, can be divided into it is military with it is civilian.Military side
Face, unmanned plane are divided into reconnaissance plane and target drone；Civilian aspect, unmanned plane add industrial application, are that unmanned plane has really just needed；Exist at present
It takes photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The application in road, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane itself
On the way, developed country also in actively extension industrial application and develops unmanned air vehicle technique, it is seen that unmanned plane is our daily life band
Very big convenience is carried out.
Unmanned plane currently on the market is mostly to be driven by electricity, and using battery as power source, wherein battery is divided into detachable electricity
Pond and non-dismountable battery, the energy-provision way filled respectively using replacement battery and directly.But regardless of using detachable battery still
Non-dismountable battery is unmanned plane power supply, when unmanned plane does not have electric energy under sail, because midway cannot charge, is all needed
It wants unmanned plane to make a return voyage to charge, which results in the inspection radiuses of unmanned plane to be restricted.Therefore we urgent need one
Kind can improve the control system of unmanned plane inspection radius.
Summary of the invention
Based on problem above, the present invention provides high-precision UAV Flight Control Systems, for solving existing unmanned plane
Midway cannot charge, and result in the problem of unmanned plane inspection radius is restricted.By in position in the present invention
Matrix landing platform is established, when unmanned plane does not have electricity fastly, it is flat that matrix landing can be dropped to by remote control unmanned plane
It charging on platform, such unmanned plane just no longer needs to charging of making a return voyage, so that the inspection radius of unmanned plane is bigger, it is travelable
Voyage is farther.
The present invention specifically uses following technical scheme to achieve the goals above:
High-precision UAV Flight Control System, including charging base station system and fuselage docking system, the charging base station
System includes matrix landing platform, is equipped with multiple chargeable grids on the matrix landing platform, in each grid
It is connected with charge power supply；The fuselage docking system includes the multiple ventrals touching that is mounted on body bottom surface and can dock with grid
Point.
In the present invention, staff is needed to establish the matrix landing connecting with charge power supply in position in advance flat
Platform, and the multiple ventral contacts that can be docked with grid are installed in body bottom surface；When unmanned plane does not have electricity fastly, staff can
It is dropped on matrix landing platform with remote control unmanned plane, is docked by ventral contact with grid, then pass through charge power supply
For grid energization, grid can charge to unmanned plane after being powered.After charged for unmanned plane, then remote control unmanned plane
It takes off, breaks the electricity in grid, such unmanned plane can not have to charging of making a return voyage.
It is noted here that how remote control unmanned plane rises and falls and how whether to be powered in remote control grid, pass through existing skill
Art can be realized.Advantages of the present invention essentially consists in: first is that matrix landing platform is not necessarily to special human attendance, can subtract in this way
Few corresponding human cost；Second is that unmanned plane can more quickly come into operation after charged, in this way may be used without charging of making a return voyage
To reduce my time cost accordingly；Third is that remotely carrying out quick charge to unmanned plane, the voyage of unmanned plane can be increased and patrolling
Look into radius.
As a preferred mode, the shape of the grid is square, the polarity of electrode phase in each grid
Together.
As a preferred mode, it is cornerwise to be greater than the single grid for the distance of the two neighboring ventral contact
Length.
As a preferred mode, the polarity of electrode in each grid is changeable.
As a preferred mode, the quantity of the ventral contact is four.
Beneficial effects of the present invention are as follows:
It (1), can be with when unmanned plane does not have electricity fastly by establishing matrix landing platform in position in the present invention
It being dropped on matrix landing platform and is charged by remote control unmanned plane, such unmanned plane just no longer needs to charging of making a return voyage, from
And making the inspection radius of unmanned plane bigger, travelable voyage is farther.
(2) shape of grid is square in the present invention, and the polarity of electrode in each grid is identical, can make grid in this way
Each side length it is equal, facilitate ventral contact and docked with grid.
(3) distance of two neighboring ventral contact is greater than the cornerwise length of single grid in the present invention, can protect in this way
Demonstrate,proving two ventral contacts will not drop in the same grid, can prevent two different ventral contacts from dropping to the same net
Short circuit occurs in lattice.
(4) polarity of electrode in the present invention in each grid is changeable, each before unmanned plane drops to matrix landing platform
It is not charged in grid, after unmanned plane drops on matrix landing platform, further according to actual bit of the ventral electric shock in grid
The polarity for remotely adjusting electrode in grid is set, unmanned plane can be filled without adjusting the state of unmanned plane landing in this way
Electricity, operation is simpler, is remotely adjusted according to the physical location that unmanned plane lands it is noted here that can be realized by the prior art
Polarity of electrode in whole grid, and therefore not to repeat here.
(5) quantity of ventral contact is four in the present invention, can more quickly charge, subtract for unmanned plane in this way
Corresponding time cost is lacked, has been more advantageous to during unmanned plane more quickly comes into operation.
Detailed description of the invention
Fig. 1 is three-dimensional structure sketch of the invention:
Fig. 2 is plan structure schematic diagram of the invention；
Fig. 3 is Facad structure schematic diagram of the present invention；
Fig. 4 looks up structure diagram for unmanned plane of the present invention；
Appended drawing reference: 1 matrix landing platform, 2 grids, 3 charge power supplies, 4 ventral contacts.
Specific embodiment
In order to which those skilled in the art better understand the present invention, with reference to the accompanying drawing with following embodiment to the present invention
It is described in further detail.
Embodiment 1:
As shown in Figs 1-4, high-precision UAV Flight Control System, including charging base station system and fuselage docking system,
Charging base station system includes matrix landing platform 1, and multiple chargeable grids 2, each grid are equipped on matrix landing platform 1
Charge power supply 3 is connected in 2；Fuselage docking system includes the multiple ventrals touching that is mounted on body bottom surface and can dock with grid 2
Point 4.
In the present invention, staff is needed to establish the matrix landing connecting with charge power supply 3 in position in advance
Platform 1, and the multiple ventral contacts 4 that can be docked with grid 2 are installed in body bottom surface；When unmanned plane does not have electricity fastly, work
Personnel can be dropped on matrix landing platform 1 with remote control unmanned plane, docked by ventral contact 4 with grid 2, then passed through
Charge power supply 3 is that grid 2 passes through, and grid 2 can charge to unmanned plane after being powered.After charged for unmanned plane, then far
Journey manipulation unmanned plane takes off, and breaks the electricity in grid 2, and such unmanned plane can not have to charging of making a return voyage.
It is noted here that how whether remote control unmanned plane rises and falls and how to be powered in remote control grid 2, by existing
Technology can be realized.Advantages of the present invention essentially consists in: first is that matrix landing platform 1 is not necessarily to special human attendance, in this way may be used
To reduce corresponding human cost；Second is that unmanned plane can more quickly come into operation after charged without charging of making a return voyage, this
Sample can reduce my time cost accordingly；Third is that remotely carrying out quick charge to unmanned plane, the voyage of unmanned plane can be increased
With inspection radius.
Embodiment 2:
As shown in Figs 1-4, high-precision UAV Flight Control System, including charging base station system and fuselage docking system,
Charging base station system includes matrix landing platform 1, and multiple chargeable grids 2, each grid are equipped on matrix landing platform 1
Charge power supply 3 is connected in 2；Fuselage docking system includes the multiple ventrals touching that is mounted on body bottom surface and can dock with grid 2
Point 4.
In the present embodiment, the shape of grid 2 is square, and the polarity of electrode in each grid 2 is identical, can make net in this way
Each side length of lattice 2 is equal, facilitates ventral contact 4 and docks with grid 2.
Preferably, the distance of two neighboring ventral contact 4 is greater than the cornerwise length of single grid 2, can guarantee in this way
Two ventral contacts 4 will not drop in the same grid 2, can prevent two different ventral contacts 4 from dropping to same
Short circuit occurs in grid 2.
Preferably, the polarity of electrode in each grid 2 is changeable, each net before unmanned plane drops to matrix landing platform 1
It is not charged in lattice 2, after unmanned plane drops on matrix landing platform 1, further according to actual bit of the ventral electric shock in grid 2
The polarity for remotely adjusting electrode in grid 2 is set, unmanned plane can be filled without adjusting the state of unmanned plane landing in this way
Electricity, operation is simpler, is remotely adjusted according to the physical location that unmanned plane lands it is noted here that can be realized by the prior art
Polarity of electrode in whole grid 2, and therefore not to repeat here.
Preferably, the quantity of ventral contact 4 is four, can more quickly charge, reduce for unmanned plane in this way
Corresponding time cost is more advantageous to during unmanned plane more quickly comes into operation.
The other parts of the present embodiment are same as the previously described embodiments, just repeat no more here.
It as above is the embodiment of the present invention.Design parameter in above-described embodiment and embodiment is merely to understand table
Invention verification process is stated, the scope of patent protection being not intended to limit the invention, scope of patent protection of the invention is still with it
It is all to change with equivalent structure made by specification and accompanying drawing content of the invention subject to claims, it should all similarly wrap
Containing within the scope of the present invention.
Claims (5)
1. high-precision UAV Flight Control System, it is characterised in that: described including charging base station system and fuselage docking system
Charging base station system includes matrix landing platform (1), is equipped with multiple chargeable grids on the matrix landing platform (1)
(2), charge power supply (3) are connected in each grid (2)；The fuselage docking system includes being mounted on body bottom surface and can
The multiple ventral contacts (4) docked with grid (2).
2. high-precision UAV Flight Control System according to claim 1, it is characterised in that: the shape of the grid (2)
Shape is square, and the polarity of electrode in each grid (2) is identical.
3. high-precision UAV Flight Control System according to claim 2, it is characterised in that: the two neighboring ventral
The distance of contact (4) is greater than the cornerwise length of the single grid (2).
4. high-precision UAV Flight Control System according to claim 1-3, it is characterised in that: each described
Polarity of electrode in grid (2) is changeable.
5. high-precision UAV Flight Control System according to claim 4, it is characterised in that: the ventral contact (4)
Quantity be four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910331292.XA CN110065645A (en) | 2019-04-23 | 2019-04-23 | High-precision UAV Flight Control System |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910331292.XA CN110065645A (en) | 2019-04-23 | 2019-04-23 | High-precision UAV Flight Control System |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110065645A true CN110065645A (en) | 2019-07-30 |
Family
ID=67368711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910331292.XA Pending CN110065645A (en) | 2019-04-23 | 2019-04-23 | High-precision UAV Flight Control System |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110816327A (en) * | 2019-10-18 | 2020-02-21 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN111762040A (en) * | 2020-06-07 | 2020-10-13 | 中国葛洲坝集团第一工程有限公司 | Near-field continuous navigation unmanned aerial vehicle dangerous rock monitoring system and method |
| CN111861982A (en) * | 2020-06-07 | 2020-10-30 | 中国葛洲坝集团第一工程有限公司 | Visual image monitoring and identifying system |
| WO2022144075A1 (en) * | 2020-12-29 | 2022-07-07 | Abb Schweiz Ag | Charging of an agv |
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| WO2016113766A1 (en) * | 2015-01-12 | 2016-07-21 | Sequoia Automation S.R.L. | Electrically charging system for drones |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110816327A (en) * | 2019-10-18 | 2020-02-21 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN110816327B (en) * | 2019-10-18 | 2023-04-14 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN111762040A (en) * | 2020-06-07 | 2020-10-13 | 中国葛洲坝集团第一工程有限公司 | Near-field continuous navigation unmanned aerial vehicle dangerous rock monitoring system and method |
| CN111861982A (en) * | 2020-06-07 | 2020-10-30 | 中国葛洲坝集团第一工程有限公司 | Visual image monitoring and identifying system |
| CN111762040B (en) * | 2020-06-07 | 2023-08-18 | 中国葛洲坝集团第一工程有限公司 | Near-field relay unmanned aerial vehicle dangerous rock monitoring system and method |
| CN111861982B (en) * | 2020-06-07 | 2024-03-12 | 中国葛洲坝集团第一工程有限公司 | Visual image monitoring and identifying system |
| WO2022144075A1 (en) * | 2020-12-29 | 2022-07-07 | Abb Schweiz Ag | Charging of an agv |
| CN116635265A (en) * | 2020-12-29 | 2023-08-22 | Abb瑞士股份有限公司 | AGV charging |
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Application publication date: 20190730 |