CN113212778A - Unmanned aerial vehicle's descending recovery system - Google Patents
Unmanned aerial vehicle's descending recovery system Download PDFInfo
- Publication number
- CN113212778A CN113212778A CN202110491558.4A CN202110491558A CN113212778A CN 113212778 A CN113212778 A CN 113212778A CN 202110491558 A CN202110491558 A CN 202110491558A CN 113212778 A CN113212778 A CN 113212778A
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- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- nest
- control module
- recovery system
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- 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
- 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
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- 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
- B60L53/30—Constructional details of charging stations
-
- 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
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
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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
- 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
- Y02T90/12—Electric charging stations
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a landing recovery system of an unmanned aerial vehicle, which comprises: the unmanned aerial vehicle exposed by the nest and the charger socket is modified; the nest includes: the tapered unmanned aerial vehicle parking apron is used for receiving the landed unmanned aerial vehicle; the charging integration box is used for controlling output current so as to realize power supply to the unmanned aerial vehicle; magnetism is inhaled formula and is charged interface for connect unmanned aerial vehicle's the machine socket that charges. According to the invention, the parking apron is arranged in a basin shape, the unmanned aerial vehicle lands in the parking apron, the unmanned aerial vehicle is enabled to swing to the right position under the action of the vibration hammer, in the process of swinging to the right position, the charger socket exposed by the unmanned aerial vehicle refitting is connected with the magnetic suction type charging interface, and charging operation can be carried out under the action of the charging integration box.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a landing recovery system of an unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Unmanned aerial vehicle recovery system that all unmanned aerial vehicle automation places adopted in the market reaches the purpose that makes unmanned aerial vehicle can descend to appointed unmanned aerial vehicle automatic airport accurately with the help of products such as machine vision, sensor more, what also adopt to unmanned aerial vehicle's the problem of charging is that the mode of the automatic dismouting battery of manipulator realizes, and this a series of technique leads to the price of unmanned aerial vehicle automatic airport to be high, is difficult to realize the purpose of extensive application.
Therefore, a landing recovery system for unmanned aerial vehicles is provided.
Disclosure of Invention
The invention aims to: in order to solve the problems, the landing recovery system of the unmanned aerial vehicle is provided.
In order to achieve the purpose, the invention adopts the following technical scheme:
a landing recovery system for a drone, comprising:
the unmanned aerial vehicle exposed by the nest and the charger socket is modified;
the nest includes:
the tapered unmanned aerial vehicle parking apron is used for receiving the landed unmanned aerial vehicle;
the charging integration box is used for controlling output current so as to realize power supply to the unmanned aerial vehicle;
the magnetic suction type charging interface is used for connecting a charger socket of the unmanned aerial vehicle;
the vibration hammer is used for promoting the unmanned aerial vehicle to be in a correct position so as to realize that a charger socket of the unmanned aerial vehicle is connected with the magnetic suction type charging interface;
the controller comprises a nest network module, a controller control module, a vibration hammer control module, a charging control module, an unmanned aerial vehicle control module and a nest control module.
As a further description of the above technical solution:
the controller also includes a nest top cap control module.
As a further description of the above technical solution:
the unmanned aerial vehicle parking apron is arranged in a basin shape.
In summary, due to the adoption of the technical scheme, the invention has the beneficial effects that:
according to the invention, the parking apron is arranged in a basin shape, the unmanned aerial vehicle lands in the parking apron, the unmanned aerial vehicle is enabled to swing to the right position under the action of the vibration hammer, in the process of swinging to the right position, the charger socket exposed by the unmanned aerial vehicle refitting is connected with the magnetic suction type charging interface, and charging operation can be carried out under the action of the charging integration box.
Drawings
Fig. 1 is a schematic diagram illustrating a top view of a nest provided according to an embodiment of the invention;
fig. 2 shows a schematic view of a flying process of an unmanned aerial vehicle provided according to an embodiment of the present invention
Fig. 3 shows a schematic view of a landing process of an unmanned aerial vehicle according to an embodiment of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a landing recovery system for a drone, comprising:
an exposed unmanned aerial vehicle is refitted by the nest and the charger socket, and the charger socket is positioned at the bottom of the unmanned aerial vehicle;
the nest includes:
the tapered unmanned aerial vehicle parking apron is used for receiving the landed unmanned aerial vehicle;
the charging integration box is used for controlling output current so as to supply power to the unmanned aerial vehicle, and is arranged inside the parking apron;
the magnetic attraction type charging interface is used for being connected with a charger socket of the unmanned aerial vehicle and is close to the central position of the parking apron;
the vibration hammer is used for enabling the unmanned aerial vehicle to be in a correct position so as to realize that a charger socket of the unmanned aerial vehicle is connected with a magnetic type charging interface, and the vibration hammer is installed on the outer side wall of the parking apron;
the controller comprises a nest network module, a controller control module, a vibration hammer control module, a charging control module, an unmanned aerial vehicle control module and a nest control module.
The controller also comprises a nest top cover control module which is used for controlling the opening and closing of the nest top cover.
The unmanned aerial vehicle air park is the basin form setting, and at the in-process of vibration cone vibration, unmanned aerial vehicle draws close to the center department on air park.
The working principle is as follows:
when the unmanned aerial vehicle is flying: firstly, a controller can issue an instruction to the nest network module through the server terminal, and the nest network module can send an instruction to control the start of the nest top cover and the start of the unmanned aerial vehicle through the nest top cover control module and the unmanned aerial vehicle control module of the nest. And after the unmanned aerial vehicle and the nest are completely started, the state of the unmanned aerial vehicle and the nest can be displayed by returning a signal to the server terminal through the controller network module. If unmanned aerial vehicle and nest state are good, accessible server terminal sends for nest control module and patrols and examines the task, can transmit the task for unmanned aerial vehicle control module after the nest network module receives the task, unmanned aerial vehicle control module can obtain current unmanned aerial vehicle electric quantity continuation of the journey data from unmanned aerial vehicle remote control handle after receiving the task, if battery continuation of the journey time is enough, unmanned aerial vehicle control module can send the task for unmanned aerial vehicle, unmanned aerial vehicle takes off and carries out the task. If the endurance time is not allowed, a signal is returned to the controller network module, the controller network module returns a signal to the server terminal to inform that the battery endurance time is insufficient, and the task is waited to be executed. When the battery duration is enough, the controller control module sends an instruction to the server terminal through the controller network module to inquire whether to continue to execute the waiting task, if the waiting task is selected to be executed, the unmanned aerial vehicle continues to execute the task, and if the waiting task is not executed, the unmanned aerial vehicle gives up the task. And after the unmanned aerial vehicle gives up executing the waiting task, the server terminal can send the task to the unmanned aerial vehicle again.
Unmanned aerial vehicle is when descending: when the unmanned aerial vehicle executes the task, the unmanned aerial vehicle returns to land to an air park of the airfield (the error between the landing point and the takeoff point of the unmanned aerial vehicle is generally 0.1 m), after the unmanned aerial vehicle lands (the blades stop rotating), the unmanned aerial vehicle control module in the controller can acquire the current state of the unmanned aerial vehicle from the unmanned aerial vehicle control handle, when the unmanned aerial vehicle status code is 0(0 means that the unmanned aerial vehicle stops), the unmanned aerial vehicle control module acquires the current status of the charging induction module in the controller, if the state shows that the state is 0(0 represents that the unmanned aerial vehicle is not charged), the unmanned aerial vehicle control module sends an instruction to the vibration hammer control module to start the vibration hammer to enable the unmanned aerial vehicle to swing to the right position, when the magnetic type charging interface of the unmanned aerial vehicle is connected with the magnetic type charging interface in the parking apron (at the moment, the unmanned aerial vehicle is in a starting state and cannot be charged), the state code of the charging control module can be changed into '1' and is transmitted back to the unmanned aerial vehicle control module and the controller network module. The unmanned aerial vehicle control module can control the vibration hammer control module, so that the vibration hammer stops vibrating. The controller network module can control the unmanned aerial vehicle handle to read the image data in the unmanned aerial vehicle and pass back to the server, and when all the image data of unmanned aerial vehicle are all obtained, the controller network module can control the unmanned aerial vehicle handle to empty the unmanned aerial vehicle memory and control the unmanned aerial vehicle to shut down. When the controller network module acquires that the state of the unmanned aerial vehicle in the unmanned aerial vehicle handle is displayed as a shutdown state, the controller network module sends an instruction to the charging control module and the nest top cover control module to charge the unmanned aerial vehicle and close the nest top cover. After the standby nest is closed, the nest network module transmits the state information back to the server terminal, and changes the state of the nest in the server terminal (changes the execution task into the waiting task).
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (3)
1. The utility model provides an unmanned aerial vehicle's descending recovery system which characterized in that includes:
the unmanned aerial vehicle exposed by the nest and the charger socket is modified;
the nest includes:
the tapered unmanned aerial vehicle parking apron is used for receiving the landed unmanned aerial vehicle;
the charging integration box is used for controlling output current so as to realize power supply to the unmanned aerial vehicle;
the magnetic suction type charging interface is used for connecting a charger socket of the unmanned aerial vehicle;
the vibration hammer is used for promoting the unmanned aerial vehicle to be in a correct position so as to realize that a charger socket of the unmanned aerial vehicle is connected with the magnetic suction type charging interface;
the controller comprises a nest network module, a controller control module, a vibration hammer control module, a charging control module, an unmanned aerial vehicle control module and a nest control module.
2. A landing recovery system for unmanned aerial vehicles according to claim 1, wherein the controller further comprises a nest top cover control module.
3. A landing recovery system for unmanned aerial vehicles according to claim 2, wherein the unmanned aerial vehicle apron is arranged in a basin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110491558.4A CN113212778A (en) | 2021-05-06 | 2021-05-06 | Unmanned aerial vehicle's descending recovery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110491558.4A CN113212778A (en) | 2021-05-06 | 2021-05-06 | Unmanned aerial vehicle's descending recovery system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113212778A true CN113212778A (en) | 2021-08-06 |
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ID=77091057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110491558.4A Withdrawn CN113212778A (en) | 2021-05-06 | 2021-05-06 | Unmanned aerial vehicle's descending recovery system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113212778A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455062A (en) * | 2022-01-04 | 2022-05-10 | 武汉理工大学 | Spherical unmanned aerial vehicle, magnetic suction type self-adaptive charging system and method |
| CN114537688A (en) * | 2022-01-18 | 2022-05-27 | 武汉汇卓航科技有限公司 | Unmanned aerial vehicle sliding platform device |
-
2021
- 2021-05-06 CN CN202110491558.4A patent/CN113212778A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455062A (en) * | 2022-01-04 | 2022-05-10 | 武汉理工大学 | Spherical unmanned aerial vehicle, magnetic suction type self-adaptive charging system and method |
| CN114537688A (en) * | 2022-01-18 | 2022-05-27 | 武汉汇卓航科技有限公司 | Unmanned aerial vehicle sliding platform device |
| CN114537688B (en) * | 2022-01-18 | 2024-04-16 | 武汉汇卓航科技有限公司 | Unmanned aerial vehicle landing platform device |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20210806 |