CN106094858A - A kind of full link control system of unmanned plane and control method thereof - Google Patents
A kind of full link control system of unmanned plane and control method thereof Download PDFInfo
- Publication number
- CN106094858A CN106094858A CN201610728136.3A CN201610728136A CN106094858A CN 106094858 A CN106094858 A CN 106094858A CN 201610728136 A CN201610728136 A CN 201610728136A CN 106094858 A CN106094858 A CN 106094858A
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- Prior art keywords
- unmanned plane
- transmission module
- earth station
- digital transmission
- control
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- 238000000034 method Methods 0.000 title claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims abstract description 59
- 238000004891 communication Methods 0.000 claims abstract description 14
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 5
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Classifications
-
- 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- 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
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Computer Networks & Wireless Communication (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
nullThe invention discloses a kind of full link control system of unmanned plane and control method thereof，Relate to unmanned plane field，Including unmanned plane and earth station，Described unmanned plane and earth station's radio communication connect，Described unmanned plane is provided with figure transmission module I and digital transmission module I，Described earth station is provided with figure transmission module II、Digital transmission module II and control module，Described figure transmission module I includes visible ray load and infrared light load，Described digital transmission module I includes that data send and receives unit，Described figure transmission module II includes visible ray display unit and infrared light display unit，Described digital transmission module II includes destination navigation elements、Parameter set unit and control instruction unit，Described control module includes flight control units，The full link control system of unmanned plane of the present invention，Achieve getting through of all communication links with unmanned plane，Greatly facilitate the control of unmanned plane，Decrease cost of labor when performing aerial mission and resources costs.
Description
Technical field
The present invention relates to unmanned plane field, particularly to a kind of full link control system of unmanned plane and control method thereof.
Background technology
Unmanned plane does not has complete unmanned plane communication link system at present.When performing unmanned plane during flying task, or
A lot of functions can not be used, or the control module that can only add other carries out many people operation, thus to UAV Flight Control
Add many human costs and resources costs, and operation contradiction often occurs when many people operate, reduce execution flight and appoint
The efficiency of business.
Summary of the invention
The technical problem to be solved is to provide a kind of full link control system of unmanned plane and control method thereof, with
Solve the above-mentioned multinomial defect caused in prior art.
For achieving the above object, the present invention provides following technical scheme: a kind of full link control system of unmanned plane, including
Unmanned plane and earth station, described unmanned plane and earth station's radio communication connect, and described unmanned plane is provided with figure transmission module I sum and passes
Module I, described earth station is provided with figure transmission module II, digital transmission module II and control module, and described figure transmission module I includes visible ray
Load and infrared light load, described digital transmission module I includes that data send and receives unit, and described figure transmission module II includes that visible ray shows
Show that unit and infrared light display unit, described digital transmission module II include destination navigation elements, parameter set unit and control instruction
Unit, described control module includes flight control units.
Preferably, the digital transmission module II in described earth station and the digital transmission module I on unmanned plane is by MAVLink communication even
Connect.
The control method of the full link control system of a kind of unmanned plane, comprises the following steps:
(1) unmanned plane is by the visible ray load of figure transmission module I and infrared light load Real-time Collection photo and video recording, and passes
Pass the figure transmission module II of earth station, show image by visible ray display unit and infrared light display unit；
(2) the digital transmission module II of earth station is by the mutual communication of digital transmission module I of MAVLink with unmanned plane, earth station
The destination navigation elements of digital transmission module II, parameter set unit and control instruction unit by MAVLink send command messages to
Unmanned plane, the data in the digital transmission module I of unmanned plane send and receive unit reception command messages, and then control the flight of unmanned plane
Action and parameter are arranged；
(3) unmanned plane pitching, driftage, roll and throttle are controlled by control module.
Above technical scheme is used to provide the benefit that: the full link control system of unmanned plane of the present invention, it is achieved that with nothing
Getting through of man-machine all communication links, greatly facilitates the control of unmanned plane, decrease perform aerial mission time artificial
Cost and resources costs.
Accompanying drawing explanation
Fig. 1 is the theory diagram of the present invention.
Detailed description of the invention
Describe the preferred embodiment of the present invention below in conjunction with the accompanying drawings in detail.
Fig. 1 shows the detailed description of the invention of the present invention: a kind of full link control system of unmanned plane, including unmanned plane and ground
Standing, described unmanned plane and earth station's radio communication connect, and described unmanned plane is provided with figure transmission module I and digital transmission module I, describedly
Station, face is provided with figure transmission module II, digital transmission module II and control module, and described figure transmission module I includes visible ray load and infrared light
Load, described digital transmission module I includes that data send and receives unit, and described figure transmission module II includes visible ray display unit and infrared
Light display unit, described digital transmission module II includes destination navigation elements, parameter set unit and control instruction unit, described control
Module includes flight control units.
In the present embodiment, the digital transmission module II in described earth station is led to by MAVLink with the digital transmission module I on unmanned plane
News connect.
The control method of the full link control system of a kind of unmanned plane, comprises the following steps:
(1) unmanned plane is by the visible ray load of figure transmission module I and infrared light load Real-time Collection photo and video recording, and passes
Pass the figure transmission module II of earth station, show image by visible ray display unit and infrared light display unit；
(2) the digital transmission module II of earth station is by the mutual communication of digital transmission module I of MAVLink with unmanned plane, earth station
The destination navigation elements of digital transmission module II, parameter set unit and control instruction unit by MAVLink send command messages to
Unmanned plane, the data in the digital transmission module I of unmanned plane send and receive unit reception command messages, and then control the flight of unmanned plane
Action and parameter are arranged；
(3) unmanned plane pitching, driftage, roll and throttle are controlled by control module.
Based on above-mentioned, the full link control system of unmanned plane of the present invention, unmanned plane is by the visible ray load of figure transmission module I
With infrared light load Real-time Collection photo and video recording, and pass to the figure transmission module II of earth station, by visible ray display unit
Image is shown with infrared light display unit；The digital transmission module II of earth station is mutual with the digital transmission module I of unmanned plane by MAVLink
Communication, the destination navigation elements of the digital transmission module II of earth station, parameter set unit and control instruction unit are sent out by MAVLink
Sending command messages to unmanned plane, the data in the digital transmission module I of unmanned plane send and receive unit reception command messages, and then control
The flare maneuver of unmanned plane and parameter are arranged；Unmanned plane pitching, driftage, roll and throttle is controlled by control module, this invention,
Achieve getting through of all communication links with unmanned plane, greatly facilitate the control of unmanned plane, decrease execution flight and appoint
Cost of labor during business and resources costs.
Above-described is only the preferred embodiment of the present invention, it is noted that for those of ordinary skill in the art
For, without departing from the concept of the premise of the invention, it is also possible to make some deformation and improvement, these broadly fall into the present invention
Protection domain.
Claims (3)
1. the full link control system of unmanned plane, including unmanned plane and earth station, described unmanned plane and earth station's radio communication
Connect, it is characterised in that: described unmanned plane is provided with figure transmission module I and digital transmission module I, and described earth station is provided with figure transmission module
II, digital transmission module II and control module, described figure transmission module I includes visible ray load and infrared light load, described digital transmission module I
Sending including data and receive unit, described figure transmission module II includes visible ray display unit and infrared light display unit, described number
Transmission module II includes destination navigation elements, parameter set unit and control instruction unit, and described control module includes flight control
Unit.
The full link control system of unmanned plane the most according to claim 1, it is characterised in that: the number in described earth station passes mould
Block II is connected by MAVLink communication with the digital transmission module I on unmanned plane.
3. the control method of the full link control system of unmanned plane as claimed in claim 1, it is characterised in that: include following
Step:
(1) unmanned plane is by the visible ray load of figure transmission module I and infrared light load Real-time Collection photo and video recording, and passes to
The figure transmission module II of earth station, shows image by visible ray display unit and infrared light display unit；
(2) the digital transmission module II of earth station is by the mutual communication of digital transmission module I of MAVLink with unmanned plane, the number biography of earth station
The destination navigation elements of module ii, parameter set unit and control instruction unit send command messages to unmanned by MAVLink
Machine, the data in the digital transmission module I of unmanned plane send and receive unit reception command messages, and then control the flare maneuver of unmanned plane
Arrange with parameter；
(3) unmanned plane pitching, driftage, roll and throttle are controlled by control module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610728136.3A CN106094858A (en) | 2016-08-26 | 2016-08-26 | A kind of full link control system of unmanned plane and control method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610728136.3A CN106094858A (en) | 2016-08-26 | 2016-08-26 | A kind of full link control system of unmanned plane and control method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106094858A true CN106094858A (en) | 2016-11-09 |
Family
ID=57225123
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610728136.3A Pending CN106094858A (en) | 2016-08-26 | 2016-08-26 | A kind of full link control system of unmanned plane and control method thereof |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106972633A (en) * | 2017-05-09 | 2017-07-21 | 广东容祺智能科技有限公司 | A kind of power patrol unmanned chain road relay system |
| CN107121987A (en) * | 2017-06-08 | 2017-09-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multiterminal remotely continue the chain-circuit system of control |
| ES2673445A1 (en) * | 2016-12-21 | 2018-06-21 | Ismael MONTES RUIZ | STATION FOR UNDERGROUND AERIAL VEHICLES (Machine-translation by Google Translate, not legally binding) |
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| CN104538899A (en) * | 2015-01-19 | 2015-04-22 | 中兴长天信息技术(北京)有限公司 | Wireless-transmission-based unmanned aerial vehicle platform for power line inspection |
| CN104950906A (en) * | 2015-06-15 | 2015-09-30 | 中国人民解放军国防科学技术大学 | Unmanned aerial vehicle remote measuring and control system and method based on mobile communication network |
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| CN105487518A (en) * | 2015-12-31 | 2016-04-13 | 江苏首控制造技术有限公司 | Four-axis unmanned-aerial-vehicle flight control system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| ES2673445A1 (en) * | 2016-12-21 | 2018-06-21 | Ismael MONTES RUIZ | STATION FOR UNDERGROUND AERIAL VEHICLES (Machine-translation by Google Translate, not legally binding) |
| CN106972633A (en) * | 2017-05-09 | 2017-07-21 | 广东容祺智能科技有限公司 | A kind of power patrol unmanned chain road relay system |
| CN107121987A (en) * | 2017-06-08 | 2017-09-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multiterminal remotely continue the chain-circuit system of control |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161109 |
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| RJ01 | Rejection of invention patent application after publication |