CN105892492A - Unmanned aerial vehicle communication control method and device - Google Patents

Unmanned aerial vehicle communication control method and device Download PDF

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Publication number
CN105892492A
CN105892492A CN201610402200.9A CN201610402200A CN105892492A CN 105892492 A CN105892492 A CN 105892492A CN 201610402200 A CN201610402200 A CN 201610402200A CN 105892492 A CN105892492 A CN 105892492A
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CN
China
Prior art keywords
unmanned plane
information
antenna
control terminal
primary importance
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Pending
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CN201610402200.9A
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Chinese (zh)
Inventor
郝祁
兰功金
卜亚圣
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Southwest University of Science and Technology
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Southwest University of Science and Technology
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Publication date
Application filed by Southwest University of Science and Technology filed Critical Southwest University of Science and Technology
Priority to CN201610402200.9A priority Critical patent/CN105892492A/en
Publication of CN105892492A publication Critical patent/CN105892492A/en
Priority to PCT/CN2016/102118 priority patent/WO2017211030A1/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08CTRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
    • G08C17/00Arrangements for transmitting signals characterised by the use of a wireless electrical link
    • G08C17/02Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link

Abstract

The invention discloses an unmanned aerial vehicle communication control method. The unmanned aerial vehicle communication method comprises the following steps: reading first position information in a positioning module and first antenna angle information indicated by an electronic compass by a control terminal; according to the first position information and received second position information of an unmanned aerial vehicle, calculating so as to obtain relative position of the unmanned aerial vehicle relative to the control terminal; according to the first antenna angle information and the relative position of the unmanned aerial vehicle relative to the control terminal, generating a control signal for controlling a driving module to drive a first antenna to point to the unmanned aerial vehicle. By adopting the scheme, the communication power consumption of the unmanned aerial vehicle and the control terminal can be reduced, the endurance capacity of the unmanned aerial vehicle is improved, the communication distance can be increased, and the communication interference of communication signals to an ambient environment can be also reduced.

Description

A kind of UAV Communication control method and device
Technical field
The present embodiments relate to unmanned air vehicle technique, particularly relate to a kind of UAV Communication control method and device.
Background technology
Unmanned plane can control terminal communicate with ground in real time in flight course, flies as controlled terminal transmission Row instruction is to control the flight of unmanned plane, and unmanned plane sends the image of its shooting, video to controlling terminal to deposit Store up or directly display.
Existing unmanned plane, in communication process, uses traditional omnidirectional antenna transmitting-receiving signal of communication (as controlled Signal, the number number of delivering a letter, the figure number of delivering a letter).I.e. controlling terminal uses omnidirectional antenna omnibearing to spatial emission Signal of communication, unmanned plane carries out signal reception in the effective communication distance controlling terminal signaling.Unmanned plane is also By omnidirectional antenna to the comprehensive signal of spatial emission, control terminal and launch the efficient communication of signal at unmanned plane Return signal apart from interior reception unmanned plane.
Owing to unmanned plane belongs to point-to-point communication with controlling communicating of terminal, prior art uses omnidirectional antenna It is big, apart from short and disturb big shortcoming to there is communication power consumption in the mode of transmitting-receiving signal of communication.
Summary of the invention
The present invention provides a kind of UAV Communication control method and device, to realize unmanned plane and to control terminal Communication power consumption reduces, and improves the flying power of unmanned plane, and communication distance increases simultaneously, also reduces communication The signal Communication Jamming to surrounding enviroment.
First aspect, embodiments provides a kind of UAV Communication control method, including:
Control terminal and read the primary importance information in locating module and the first antenna angle indicated by electronic compass Degree information;
Second position information according to described primary importance information with the unmanned plane received is calculated described nothing The man-machine relative position relative to described control terminal;
According to described first antenna angle information and described unmanned plane relative to the phase para-position of described control terminal Put, generate control signal to control to drive module drive first antenna to point to described unmanned plane.
Second aspect, the embodiment of the present invention additionally provides a kind of UAV Communication control method, including:
Unmanned plane reads the second position information in positioning unit and the second antenna indicated by the second electronic compass Angle information;
Primary importance information according to described second position information with the control terminal received is calculated described Control the terminal relative position relative to described unmanned plane;
According to described second aerial angle information and described control terminal relative to the phase para-position of described unmanned plane Put, generate control signal to control drive unit drives the second antenna and point to described control terminal.
The third aspect, the embodiment of the present invention additionally provides a kind of UAV Communication and controls device, including:
Locating module, for obtaining the primary importance information controlling terminal;
Electronic compass, is used for obtaining first antenna angle information;
Controller, is used for reading described primary importance information and described first antenna angle information, and according to institute State primary importance information and the second position information of unmanned plane that receives be calculated described unmanned plane relative to The relative position of described control terminal, and according to described first antenna angle information and described unmanned plane relative to The relative position of described control terminal, generates control signal;
Drive module, for driving first antenna to point to described unmanned plane, Qi Zhongsuo according to described control signal State locating module, electronic compass is connected with controller respectively with driving module.
Fourth aspect, the embodiment of the present invention additionally provides a kind of UAV Communication and controls device, including:
Positioning unit, for obtaining the second position information of unmanned plane;
Second electronic compass, for obtaining the second aerial angle information;
Controller unit, is used for reading described second position information and described second aerial angle information, and root It is calculated described control eventually according to described second position information and the primary importance information of the control terminal received Hold the relative position relative to described unmanned plane, and whole according to described second aerial angle information and described control Hold the relative position relative to described unmanned plane, generate control signal;
Driver element, for driving the second antenna to point to described unmanned plane, Qi Zhongsuo according to described control signal State positioning unit, the second electronic compass is connected with controller respectively with driver element.
The present invention reads indicated by the primary importance information in locating module and electronic compass by controlling terminal First antenna angle information, according to the second position information of described primary importance information with the unmanned plane received It is calculated the described unmanned plane relative position relative to described control terminal, according to described first antenna angle Information relative to the relative position of described control terminal, generates control signal to control to drive with described unmanned plane Module drive first antenna points to described unmanned plane, solves unmanned plane and control terminal in prior art and uses The omnidirectional antenna transmitting-receiving communication power consumption brought of signal of communication is big, apart from short and disturb high problem so that nothing Man-machine and control terminal communication power consumption reduces, and improves the flying power of unmanned plane, and communication distance increases simultaneously Greatly, the signal of communication Communication Jamming to surrounding enviroment is also reduced.
Accompanying drawing explanation
The flow chart of the UAV Communication control method that Fig. 1 provides for the embodiment of the present invention one;
The flow chart of the UAV Communication control method that Fig. 2 provides for the embodiment of the present invention two;
Fig. 3 points to and the relation schematic diagram of unmanned plane position for the antenna that the embodiment of the present invention two provides;
The schematic diagram that angle α is decomposed that Fig. 4 provides for the embodiment of the present invention two;
The flow chart of the UAV Communication control method that Fig. 5 provides for the embodiment of the present invention three;
Fig. 6 controls the structure chart of device for the UAV Communication that the embodiment of the present invention four provides;
The structural diagrams that Fig. 7 controls device for the UAV Communication that the embodiment of the present invention six provides is intended to;
The unmanned plane that Fig. 8 provides for the embodiment of the present invention six is by showing of controlling that device controls that beam antenna moves It is intended to.
Detailed description of the invention
The present invention is described in further detail with embodiment below in conjunction with the accompanying drawings.It is understood that this Specific embodiment described by place is used only for explaining the present invention, rather than limitation of the invention.The most also need It is noted that for the ease of describing, accompanying drawing illustrate only part related to the present invention and not all knot Structure.
Embodiment one
The flow chart of the UAV Communication control method that Fig. 1 provides for the embodiment of the present invention one, the present embodiment can Being applicable to control terminal and unmanned plane and carry out the situation of communication, the method can be by controlling the control of terminal such as ground Platform performs, and specifically includes following steps:
Step 101, control terminal read indicated by the primary importance information in locating module and electronic compass First antenna angle information.
Wherein, locating module is integrated in control terminal, can obtain the positional information of this control terminal in real time, This locating module optional uses GPS (Global Positioning System, global positioning system) side Formula positions.Locating module obtain primary importance information can real-time Transmission to control terminal controller in. Electronic compass, for indicating the angle of first antenna, controls the angle information that terminal can be transmitted by electronic compass Obtain the angle value of first antenna.This first antenna includes beam antenna.
Step 102, calculate according to described primary importance information and the second position information of unmanned plane received Obtain the described unmanned plane relative position relative to described control terminal.
Wherein, this primary importance information i.e. controls the positional information of terminal self, exemplary Tong Guo location Module obtains controlling the latitude and longitude value residing for terminal, and control terminal carries out the real-time of the mutual unmanned plane of information It can be the latitude and longitude information value of unmanned plane that position is defined as second position information, equally this second position information, Control terminal and can get unmanned plane relative to control according to the latitude and longitude value of self-position and the latitude and longitude value of unmanned plane The relative position of terminal processed.
Step 103, according to described first antenna angle information and described unmanned plane relative to described control terminal Relative position, generate control signal with control drive module drive first antenna point to described unmanned plane.
Exemplary, after controlling the controller generation control signal of terminal, send to The Cloud Terrace drive circuit, cloud Platform drive circuit drives horizontal stage electric machine to rotate, so that first antenna points to unmanned plane.
The technical scheme of the present embodiment, controls terminal according to unmanned plane and self relative position, controls to orient Antenna moves, and points to unmanned plane in real time, sends in particular directions due to beam antenna and accepts electromagnetic wave Ability is much stronger than existing omnidirectional antenna, and capacity of resisting disturbance is higher simultaneously so that unmanned plane and control terminal Communication power consumption reduces, and improves the flying power of unmanned plane, and communication distance increases simultaneously, also reduces communication The signal Communication Jamming to surrounding enviroment.
On the basis of technique scheme, control terminal read the primary importance information in locating module and Before first antenna angle information indicated by electronic compass, also include: control terminal and send link order, Communication connection is set up with unmanned plane;Or control the link order that the terminal described unmanned plane of reception sends, and described Unmanned plane sets up communication connection.Wherein, after controlling terminal and unmanned plane initialization, begin setting up control eventually Communication link between end and unmanned plane, accordingly, when initializing, antenna is reset to predeterminated position, can Being to be reset in antenna slot.
On the basis of technique scheme, after controlling the primary importance information that terminal reads in locating module, Also include: send described primary importance information to unmanned plane.In this programme, control terminal by the position of oneself Information sends to unmanned plane, and unmanned plane can be made to use identical principle to drive the beam antenna of unmanned plane to point to Control terminal, further increase the communication efficiency controlled between terminal and unmanned plane, reduce noise jamming.
Embodiment two
The flow chart of the UAV Communication control method that Fig. 2 provides for the embodiment of the present invention two, the present embodiment exists On the basis of embodiment one, a kind of method giving concrete adjustment first antenna, including:
Step 201, control terminal read indicated by the primary importance information in locating module and electronic compass First antenna angle information.
Step 202, the foundation three-dimensional system of coordinate with described control terminal as initial point, according to described primary importance Information is calculated described unmanned plane at described three-dimensional system of coordinate with the second position information of the unmanned plane received In coordinate figure.
As it is shown on figure 3, Fig. 3 points to and the relation of unmanned plane position for the antenna that the embodiment of the present invention two provides Schematic diagram.Wherein, to control the terminal initial point as three-dimensional system of coordinate, according to the self-position controlling terminal Unmanned plane coordinate figure in this three-dimensional system of coordinate is obtained with the positional information of unmanned plane, exemplary is (x, Y, z) coordinate figure is respectively 50,50,40.
Step 203, obtain the sensing of first antenna according to described coordinate figure and described first antenna angle information Direction and the angle of described unmanned plane.
As it is shown on figure 3, obtain two according to unmanned plane at the coordinate figure of three-dimensional system of coordinate and the sensing of first antenna The angle of person is α.Accordingly, the second antenna of available unmanned plane points to and controls the angle β of terminal.
Step 204, generate control signal to control to drive the pointing direction of module drive first antenna and described The angle of unmanned plane is zero.
Concrete, the angle α in Fig. 3, during generating control signal, is decomposed into two by controller The dominant vector in direction, as shown in Figure 4, angle α is carried out point by Fig. 4 for what the embodiment of the present invention two provided The schematic diagram solved.Respectively angle α is decomposed into αxyVector sum αxzVector, controls horizontal stage electric machine simultaneously and exists respectively Xz direction rotates α 1 angle, rotates α 2 angle in xy direction, so that first antenna points to the position of unmanned plane Put.
The technical scheme of the present embodiment, controls terminal by driving antenna to point to the position of unmanned plane so that nothing Man-machine and control terminal communication power consumption reduces, and improves the flying power of unmanned plane, and communication distance increases simultaneously Greatly, the signal of communication Communication Jamming to surrounding enviroment is also reduced.
On the basis of the various embodiments described above, also include: according to described primary importance information and described second Confidence breath is calculated described control terminal and the air line distance of described unmanned plane;According to described air line distance Length is to adjust the power consumption of transport module in real time.As it is shown on figure 3, figure marked control terminal to unmanned plane Air line distance, adjust the power consumption of transport module in real time according to the length of this distance, optionally, when this away from From the power consumption of the longest increase transport module, distance is the shortest, reduces the power consumption of transport module.Concrete, can be In test process, record the relation between antenna communication power consumption and communication distance and be stored in data base, rear Continuous transmitting procedure middle controller is according to the correspondence between communication distance and the communication power consumption recorded in this data base Relation adjusts the power consumption of transport module, exemplary, and this transport module includes sum leaflet unit of figure leaflet unit.
Embodiment three
The flow chart of the UAV Communication control method that Fig. 5 provides for the embodiment of the present invention three, the present embodiment can The scheme of unmanned plane, in the present embodiment, nothing is pointed to reference to previous embodiment controls terminal control first antenna Second antenna of Human-machine Control self controls terminal with real-time sensing, specifically includes:
Step 301, unmanned plane read indicated by the second position information in positioning unit and the second electronic compass The second aerial angle information.
Step 302, according to described second position information and the primary importance information meter of control terminal that receives Calculate and obtain the described control terminal relative position relative to described unmanned plane.
Step 303, according to described second aerial angle information and described control terminal relative to described unmanned plane Relative position, generate control signal with control drive unit drives the second antenna point to described control terminal.
The technical scheme that the present embodiment provides so that the communication power consumption of unmanned plane and control terminal reduces, and improves The flying power of unmanned plane, communication distance increases simultaneously, also reduces signal of communication and leads to surrounding enviroment Letter interference.
On the basis of technique scheme, read the second position information in positioning unit and the at unmanned plane Before the second aerial angle information indicated by two electronic compass, also include: unmanned plane sends link order, Communication connection is set up with controlling terminal;Or unmanned plane receives the link order that described control terminal sends, and institute State control terminal and set up communication connection.
On the basis of technique scheme, after the second position information in unmanned plane reads positioning unit, Also include: send described second position information to controlling terminal.
On the basis of technique scheme, according to described second position information and the control terminal received Primary importance information is calculated described control terminal and includes relative to the relative position of described unmanned plane: set up Three-dimensional system of coordinate with described unmanned plane as initial point, whole according to described second position information and the control received The primary importance information of end is calculated described control terminal coordinate figure in described three-dimensional system of coordinate;According to Described coordinate figure and described second aerial angle information obtain the pointing direction of the second antenna and described control terminal Angle.
On the basis of technique scheme, generate control signal and refer to control drive unit drives the second antenna Include to described control terminal: generate control signal to control the pointing direction of drive unit drives the second antenna It is zero with the angle of described control terminal.
On the basis of technique scheme, also include: according to described second position information and described first Confidence breath is calculated described unmanned plane and the air line distance of described control terminal;According to described air line distance Length is to adjust the power consumption of transmission unit in real time.
Embodiment four
Fig. 6 controls the structure chart of device for the UAV Communication that the embodiment of the present invention four provides, and specifically includes:
Locating module 1, for obtaining the primary importance information controlling terminal;
Electronic compass 2, is used for obtaining first antenna angle information;
Controller 3, is used for reading described primary importance information and described first antenna angle information, and according to It is relative that described primary importance information is calculated described unmanned plane with the second position information of the unmanned plane received In the relative position of described control terminal and relative with described unmanned plane according to described first antenna angle information In the relative position of described control terminal, generate control signal;
Drive module 4, for driving first antenna to point to described unmanned plane, wherein according to described control signal Described locating module, electronic compass are connected with controller respectively with driving module.
The technical scheme of the present embodiment makes unmanned plane and controls the communication power consumption reduction of terminal, improves unmanned The flying power of machine, communication distance increases simultaneously, also reduces the signal of communication Communication Jamming to surrounding enviroment.
On the basis of technique scheme, described controller specifically for: set up with described control terminal be The three-dimensional system of coordinate of initial point, according to the second position information of described primary importance information with the unmanned plane received It is calculated described unmanned plane coordinate figure in described three-dimensional system of coordinate;According to described coordinate figure and described One aerial angle information obtains pointing direction and the angle of described unmanned plane of first antenna.
On the basis of technique scheme, described controller is additionally operable to: according to described primary importance information and Described second position information is calculated described control terminal and the air line distance of described unmanned plane;According to described The length of air line distance is to adjust the power consumption of transport module in real time, and described transport module is connected with described controller.
Embodiment five
Present embodiments provide a kind of UAV Communication and control device, specifically include:
Positioning unit, for obtaining the second position information of unmanned plane;
Second electronic compass, for obtaining the second aerial angle information;
Controller unit, is used for reading described second position information and described second aerial angle information, and root It is calculated described control eventually according to described second position information and the primary importance information of the control terminal received Hold the relative position relative to described unmanned plane, and whole according to described second aerial angle information and described control Hold the relative position relative to described unmanned plane, generate control signal;
Driver element, for driving the second antenna to point to described unmanned plane, Qi Zhongsuo according to described control signal State positioning unit, the second electronic compass is connected with controller respectively with driver element.
The technical scheme of the present embodiment makes unmanned plane and controls the communication power consumption reduction of terminal, improves unmanned The flying power of machine, communication distance increases simultaneously, also reduces the signal of communication Communication Jamming to surrounding enviroment.
On the basis of technique scheme, described controller specifically for: setting up is former with described unmanned plane The three-dimensional system of coordinate of point, according to the primary importance information of described second position information with the control terminal received It is calculated described control terminal coordinate figure in described three-dimensional system of coordinate;According to described coordinate figure and described Second aerial angle information obtains pointing direction and the angle of described control terminal of the second antenna.
On the basis of technique scheme, described controller is additionally operable to: according to described second position information and Described primary importance information is calculated described unmanned plane and the air line distance of described control terminal;According to described The length of air line distance is to adjust the power consumption of transmission unit in real time, and described transmission unit is connected with described controller.
The said goods can perform the method that any embodiment of the present invention is provided, and possesses the corresponding merit of execution method Can module and beneficial effect.
Embodiment six
The present embodiment can be based on above-described embodiment, it is provided that a kind of preferred embodiment.Fig. 7 is the present invention The UAV Communication that embodiment six provides controls the structural diagrams of device and is intended to.As it is shown in fig. 7, control terminal To carry out information by respective beam antenna mutual with unmanned plane.Initial phase, unmanned plane and control terminal Set up communication link, position the positional information of self by respective GPS and be transferred to the other side.Concrete, GPS is connected with controller, and location information is transferred to controller, and electronic compass is transferred to controller calmly simultaneously To the angle information of antenna, controller sends the signal to number biography/figure and passes transceiver module and complete through beam antenna Alternately.When unmanned plane The Cloud Terrace is believed with the positional information position relative with the other side controlling all to obtain in terminal self After breath, controller sends control signal and drives The Cloud Terrace to drive module to move accordingly so that orienting sky to control The Cloud Terrace Line points to the other side.Exemplary, as shown in Figure 8, the unmanned plane that Fig. 8 provides for the embodiment of the present invention six leads to Cross and control the schematic diagram that device control beam antenna moves.Corresponding, control terminal and control by controlling device The structure of beam antenna is identical with this.Wherein, The Cloud Terrace be positioned on foot rest can laterally, vertical rotating, orient sky Line is arranged on The Cloud Terrace, can move with the rotation of The Cloud Terrace, The Cloud Terrace opposite side be equipped with battery, electronic compass, Controller, GPS, number pass the/module such as figure biography and drive circuit.
The technical scheme that the present embodiment provides, unmanned plane and control terminal are in communication process, each via cloud The movement of platform makes beam antenna point to the other side so that the communication power consumption of unmanned plane and control terminal reduces, and carries The high flying power of unmanned plane, communication distance increases simultaneously, also reduces signal of communication to surrounding enviroment Communication Jamming.
Note, above are only presently preferred embodiments of the present invention and institute's application technology principle.Those skilled in the art It will be appreciated that the invention is not restricted to specific embodiment described here, can enter for a person skilled in the art Row various obvious changes, readjust and substitute without departing from protection scope of the present invention.Therefore, though So by above example, the present invention is described in further detail, but the present invention be not limited only to Upper embodiment, without departing from the inventive concept, it is also possible to include other Equivalent embodiments more, And the scope of the present invention is determined by scope of the appended claims.

Claims (10)

1. a UAV Communication control method, it is characterised in that including:
Control terminal and read the primary importance information in locating module and the first antenna angle indicated by electronic compass Degree information;
Second position information according to described primary importance information with the unmanned plane received is calculated described nothing The man-machine relative position relative to described control terminal;
According to described first antenna angle information and described unmanned plane relative to the phase para-position of described control terminal Put, generate control signal to control to drive module drive first antenna to point to described unmanned plane.
Method the most according to claim 1, it is characterised in that read in locating module controlling terminal Primary importance information and electronic compass indicated by first antenna angle information before, also include:
Control terminal and send link order, and unmanned plane sets up communication connection;Or control the terminal described nothing of reception The link order of man-machine transmission, and the foundation communication connection of described unmanned plane.
Method the most according to claim 1, it is characterised in that read in locating module controlling terminal Primary importance information after, also include:
Send described primary importance information to unmanned plane.
Method the most according to claim 1, it is characterised in that according to described primary importance information and connecing The second position information of the unmanned plane received is calculated relative relative to described control terminal of described unmanned plane Position includes:
Set up the three-dimensional system of coordinate with described control terminal as initial point, according to described primary importance information and reception To the second position information of unmanned plane be calculated described unmanned plane coordinate in described three-dimensional system of coordinate Value;
The pointing direction of first antenna and described is obtained according to described coordinate figure and described first antenna angle information The angle of unmanned plane.
Method the most according to claim 4, it is characterised in that generate control signal to control to drive mould Block drives the first antenna described unmanned plane of sensing to include:
Generate control signal to control to drive pointing direction and the folder of described unmanned plane of module drive first antenna Angle is zero.
6. according to the method according to any one of claim 1-5, it is characterised in that also include:
It is calculated described control terminal and described according to described primary importance information and described second position information The air line distance of unmanned plane;
Length according to described air line distance is to adjust the power consumption of transport module in real time.
7. a UAV Communication control method, it is characterised in that including:
Unmanned plane reads the second position information in positioning unit and the second antenna indicated by the second electronic compass Angle information;
Primary importance information according to described second position information with the control terminal received is calculated described Control the terminal relative position relative to described unmanned plane;
According to described second aerial angle information and described control terminal relative to the phase para-position of described unmanned plane Put, generate control signal to control drive unit drives the second antenna and point to described control terminal.
Method the most according to claim 7, it is characterised in that according to described second position information and connecing The primary importance information of the control terminal received is calculated the described control terminal phase relative to described unmanned plane Position is included:
Set up three-dimensional system of coordinate with described unmanned plane as initial point, according to described second position information with receive The primary importance information of control terminal be calculated described control terminal coordinate in described three-dimensional system of coordinate Value;
The pointing direction of the second antenna and described is obtained according to described coordinate figure and described second aerial angle information Control the angle of terminal.
9. a UAV Communication controls device, it is characterised in that including:
Locating module, for obtaining the primary importance information controlling terminal;
Electronic compass, is used for obtaining first antenna angle information;
Controller, is used for reading described primary importance information and described first antenna angle information, and according to institute State primary importance information and the second position information of unmanned plane that receives be calculated described unmanned plane relative to The relative position of described control terminal, and according to described first antenna angle information and described unmanned plane relative to The relative position of described control terminal, generates control signal;
Drive module, for driving first antenna to point to described unmanned plane, Qi Zhongsuo according to described control signal State locating module, electronic compass is connected with controller respectively with driving module.
10. a UAV Communication controls device, it is characterised in that including:
Positioning unit, for obtaining the second position information of unmanned plane;
Second electronic compass, for obtaining the second aerial angle information;
Controller unit, is used for reading described second position information and described second aerial angle information, and root It is calculated described control eventually according to described second position information and the primary importance information of the control terminal received Hold the relative position relative to described unmanned plane, and whole according to described second aerial angle information and described control Hold the relative position relative to described unmanned plane, generate control signal;
Driver element, for driving the second antenna to point to described unmanned plane, Qi Zhongsuo according to described control signal State positioning unit, the second electronic compass is connected with controller respectively with driver element.
CN201610402200.9A 2016-06-07 2016-06-07 Unmanned aerial vehicle communication control method and device Pending CN105892492A (en)

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PCT/CN2016/102118 WO2017211030A1 (en) 2016-06-07 2016-10-14 Communications control method and device for unmanned aerial vehicle

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