CN107945481A - Unmanned controller and its display methods - Google Patents
Unmanned controller and its display methods Download PDFInfo
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- CN107945481A CN107945481A CN201711214504.3A CN201711214504A CN107945481A CN 107945481 A CN107945481 A CN 107945481A CN 201711214504 A CN201711214504 A CN 201711214504A CN 107945481 A CN107945481 A CN 107945481A
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- remote controler
- aircraft
- display screen
- slide bar
- areas
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Classifications
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- 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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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/60—Control of cameras or camera modules
- H04N23/66—Remote control of cameras or camera parts, e.g. by remote control devices
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
- H04N7/185—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source from a mobile camera, e.g. for remote control
Abstract
The present invention discloses a kind of unmanned controller and its display methods, control unit including remote controler housing and in remote controler housing, it is characterized in that, the positive center section of the remote controler housing sets display screen, in display screen both sides difference Setting pattern conversion slide bar, throttle slide bar, in the downside of display screen, button keyboard is set, remote controler housing is also on the upper left side of display screen, upper right side is respectively arranged to receive the antennal interface for sending control data, the shutter release taken pictures, throttle joystick is set adjacent to pattern conversion slide bar, posture control stick is set adjacent to the throttle slide bar, charging interface is provided with front side of remote controler housing, power switch.Topology layout of the present invention is reasonable, proper so that flexible to operation with reference to each button of remote controler, switch, rocking bar layout.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of unmanned controller and its display methods.
Background technology
Unmanned plane is also known as unmanned vehicle, is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft.With the development of science and technology, more and more users have touched unmanned plane, the nothing using multi-rotor aerocraft as representative
It is man-machine gradually to enter ordinary consumer field from professional consumer domain.At present, the remote control used in domestic rotor unmanned aircraft
Device controls separated pattern using video frequency graphic monitoring and aircraft mostly, and video image cannot be carried out at the same time when operating unmanned plane
Monitoring and the various postures of aircraft control, be inconvenient using process, while existing aircraft is designed with remote controller structure
It is unreasonable so that during operating with, to operate each button and be inconvenient, action switching is dumb, be easy to cause operation and loses
The generation of the situations such as mistake.
The content of the invention
The purpose of the present invention aims to provide a kind of unmanned controller and its display methods, makes unmanned aerial vehicle (UAV) control operation more
It is convenient, and the monitoring of video image and the control of the various postures of aircraft can be carried out at the same time, to overcome deficiency of the prior art
Part.
To achieve the above object, technical solution provided by the present invention is：A kind of unmanned controller, the remote controler shell
The positive center section of body sets display screen, and in display screen both sides, difference Setting pattern changes slide bar, throttle slide bar, in display screen
Downside set button keyboard, remote controler housing be also respectively arranged in the upper left side of display screen, upper right side receive send control
The antennal interface of data processed, the shutter release taken pictures, throttle joystick are set adjacent to pattern conversion slide bar, and posture manipulates
Bar is set adjacent to the throttle slide bar, and charging interface, power switch are provided with front side of remote controler housing.
Buzzer is additionally provided with front side of remote controler housing.
Coach-student's switch, the upper right corner is set to set destination to switch in the upper left corner of remote controler housing, in remote controler housing
Lower-left or lower right the control passage switching switch of the first control passage/second is set.
In the corner of remote controler housing, corner protector is set.
The display methods of above-mentioned unmanned controller, data radio station receive aircraft section downlink data, will be from aircraft
Send back the Flight Condition Data come to export to the display screen of remote controler, correspondingly shown by display screen, it is characterised in that：
Lattice point map P areas are set in the display interface central region of rectangular display screen, aircraft orientation and aircraft are shown in P areas
Forearm is directed toward, and multiple rectangle display boxes for being used to show aircraft state information, the multiple square are set around lattice point map area
Shape display box order includes：Height A areas, navigation Mode B area, landing secondary status D areas, number of satellite F areas, signal strength are shown
Show G areas, battery status H areas, flight time J area, position coordinates M areas；The navigation Mode B area includes at least following navigation mould
Formula：INS inertial navigation systems, MAG magnetometers, GNSS Global Navigation Satellite System, WP destinations, mono- keys of HM make a return voyage.
The beneficial effects of the invention are as follows：The method of the present invention is shown by being set in the positive center section of remote controler housing
Screen, realization show navigation pattern, pressure altitude, forearm direction, cumulative flight time, grating map, its one on a remote control
Change operation interface, realize the monitoring that flight state can be carried out at the same time when operating unmanned plane and the various postures of aircraft
Control, and various functions can be set according to demand, it is very convenient using process, while it shows that topology layout is reasonable, is operating
It is proper so that flexible to operation with reference to each button of remote controler, switch, rocking bar layout during use, it will not occur to grasp by mistake
The occurrence of making.
Brief description of the drawings
Fig. 1 is unmanned controller structure diagram (front) of the present invention.
Fig. 2 is unmanned controller schematic perspective view of the present invention.
Fig. 3 is unmanned controller people display screen interface schematic diagram of the present invention.
In attached drawing, each label represents as follows：Throttle joystick 1, coach-student's switch 2, antennal interface 3, pattern conversion are slided
Bar 4, display screen 5, throttle slide bar 6, shutter release 7, destination switch 8, posture control stick 9, control passage changes switch 11, button key
Disk 12, control passage change switch (as 9 functions) 13, charging interface 15, buzzer 16, power switch 17.
Embodiment
The embodiment of the present invention is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning to end
Same or similar label represents same or similar element or has the function of same or like element.Below with reference to attached
The embodiment of figure description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that term " front and rear ", " on ", " under ", "left", "right", " vertical ",
The orientation or position relationship of the instruction such as " level ", " interior ", " outer " be based on orientation shown in the drawings or position relationship, merely to
Easy to describe the present invention and simplify description, rather than instruction or imply signified device or element must have specific orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.
In the description of the present invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should broadly understood, for example, it may be being fixedly connected.Can also be detachably connected, or be integrally connected；Can
To be mechanical connection or be electrically connected；It can be directly connected, can also be indirectly connected by intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
The concrete meaning of invention.
The present invention provides a kind of unmanned controller and its display methods, wherein, remote controler includes remote-control lever and remote control is opened
Pass, display screen, transmitter, data radio station XPEND-900A, wherein transmitter are gathered and are handled user and remote-control lever and remote control are opened
The operation of pass, generation control signal, become the flight control data of control aircraft.The data radio station XPEND- of ground remote control device
900A is used to carry out data exchange with aircraft, sends the control signals such as flight control data to aircraft, receives aircraft portion
Divide downlink data.Ground remote control device also set up display module be used for by from aircraft send back come Flight Condition Data export to
The display screen of remote controler, is correspondingly shown by display screen.It is corresponding on aircraft also to there is data radio station to be used to carry out data friendship
Change, carry-on data radio station XPEND-900B is matched with the data radio station XPEND-900A of remote controler and carried out corresponding count
According to interaction, i.e. data link is established between data radio station XPEND-900B and data radio station XPEND-900A, aircraft is based on connecing
The flare maneuver of received flight control data control unmanned plane, and correspondingly gather the status data of all parts of aircraft
Form state of flight downlink data and beam back ground.The transmitter of remote controler is carried out by USART interfaces and display screen, data radio station
Data transfer, WINCE receive serial data and show, configuration is replaced and firmware upgrade, 3 switching value passages of collection, 6 simulations
Passage, direction key signal are measured, produces 9 passage PPM signals, and reserved serial communication interface.Hereafter, unmanned plane receiver base
In the flight control data that the transmitter that data radio station XTEND-900B is received is sent, microcontroller receives and decoding control data production
The action of the flare maneuver and holder camera of the PPM signal control aircraft of each 9 passage of raw two-way.
Referring to Fig. 1-2, unmanned controller includes remote controler housing and the control unit in remote controler housing, distant
The positive center section of control device housing is provided with the display for real time inspection unmanned plane during flying state and display remote controller data
Screen 5, the front of remote controler housing is additionally provided with pattern conversion slide bar 4, throttle slide bar 6 positioned at display screen both sides, in display screen
Downside set button keyboard 12, be respectively arranged in the left upper right corner of display screen receive send control data antennal interface
3rd, the shutter release 7 taken pictures, 1 adjacent modes of throttle joystick conversion slide bar 4 are set, and posture control stick 9 is adjacent to throttle slide bar 6
Set, charging interface 15, buzzer 16, power switch 17 are provided with front side of remote controler housing.Wherein, pattern conversion slide bar 4
There are three gear selections, the conversion being respectively used between INS, MAG, GPS pattern.Throttle slide bar 6 coordinates throttle joystick to use,
It may be selected to open or close two gears of motor.Button keyboard 12 is used to control camera zoom or remote controler to set.Buzzer 16
System alarm during for dangerous situation occur.Shutter release 7 shares three gears.
The upper left corner of remote controler housing sets coach-student's switch 2, and the upper right corner sets destination to switch 8, remote controler housing
Lower left sets the first switching switch 11, and lower right sets the second switching switch 13.Coach-student's switch 2 is used to train, ground
On there are two remote controlers (trainer aircraft, student's machine) to be matched with unmanned plane receiver, when coach's remote controler switchs coach-student
When pulling out to trainer aircraft, the remote control command failure of student's machine, unmanned plane receiver receives the remote control command of trainer aircraft.Destination switch 8
There are three gears, two switching switches and the shutter release taken pictures, destination switch, posture control stick, pattern conversion slide bar or oil
Door control lever, which is used together, starts different functions.
The corner of the remote controler housing sets corner protector 14, plays protective housing, reduces housing and is collided be subject to foreign matter
Surge guard damages.
Referring to Fig. 3, the display methods of above-mentioned unmanned controller, data radio station receives aircraft section downlink data, will
The Flight Condition Data come is sent back from aircraft to export to the display screen of remote controler, is correspondingly shown by display screen, its
It is characterized in that：Lattice point map P areas are set in the display interface central region of rectangular display screen, aircraft orientation is shown in P areas
And the forearm of aircraft is directed toward, multiple rectangle display boxes for being used to show aircraft state information are set around lattice point map area,
The multiple rectangle display box order includes：Height A areas, navigation Mode B area, landing secondary status D areas, number of satellite F areas,
Signal strength shows G areas, battery status H areas, flight time J area, position coordinates M areas；The navigation Mode B area include at least with
Lower navigation pattern：INS inertial navigation systems, MAG magnetometers, GNSS Global Navigation Satellite System, WP destinations, mono- keys of HM make a return voyage.
Digital remote control is furnished with an intelligent charger, and charger has the safe interface of 7 pins, the interface and remote controler
Charging interface correspond to.After remote controler recognizes charging adapter, the LED light positioned at main panel rear can start to flicker, and give
When remote controler charges, LED light can continue to flicker, until charging complete just stops.The power switch of digital remote control is positioned at remote control
The top of device, the Position Design can prevent from accidental switching off power supply.The transmitting module of digital remote control can be according to task and ring
Border requires to set different transmission power, and user can set 100mw under more conservative environment, may noisy task
In or long-distance flight, can manually increase to 1W before unmanned plane takes off.The serial aircraft of quadrotor provides to the user
Down-transmitting data in-flight, data message are received by remote controler, and then decoding is shown on graphic user interface (GUI), allows use
Know the real-time status of aircraft in family.In Fig. 3, each region position is represented with arrow and digital code, is respectively A-P totally 16
A region, each region of graphic user interface (GUI) show that information is as follows：
A --- apart from the diagonal distance and pressure altitude of takeoff point
B --- navigation pattern
C --- virtual fence prompting
D --- landing secondary status
The direction and forearm that E --- forearm takes off are directed toward (arrow)
The figure instruction of F --- GNSS satellite quantity, positional precision and signal quality
G --- RC signal qualities and signal strength (strip and percentages)
H --- battery current voltage and figure instruction
I --- the sequence number of current controlled aircraft
J --- cumulative operating time (OT) or flight time (FT)
K --- SII functions
L --- the takeoff point on 2D grating maps
M --- the current location on X, Y-axis, and LLA coordinates
N --- the ratio of 2D grating maps
O --- graphical display of the current location of md4 series aircraft on 2D grating maps
P --- lattice point map
In B --- several different navigation patterns that can be shown in navigation mode region.Navigation pattern is according to flight progress
And GPS mass is different and different：
1) INS inertial navigation systems
Slide bar, which is shifted onto, can activate this state, this is the simplest navigation pattern that aircraft performs, and most dynamic
State.In this mode, aircraft affected by wind may shift, will on flying distance or the information of current location
It will not show, fly indoors or be subject to GPS can be proper using the pattern when disturbing.
When aircraft detects RC dropouts or do not have magnetometer, INS-red limit risks may be activated.
2) MAG magnetometers
Shift slide bar onto middle potential energy and activate this state, under the navigation pattern, aircraft can be come using the information of magnetometer
Judge the real-time direction of forearm, aircraft affected by wind may shift, on flying distance or the letter of current location
Breath will not be shown, flown indoors or be subject to GPS can be proper using the pattern when disturbing.
When aircraft detects RC dropouts or do not have magnetometer, MAG-red limit risks may be activated.
3) GNSS Global Navigation Satellite System
This is md4 series aircraft acquiescence navigation pattern set under normal operations environment, and aircraft acquiescence uses
Dynamic locks, and helps user to carry out GPS calibration when to instruction, reduces since the influence of wind causes the offset of aircraft, or
The translational speed for the instruction limitation aircraft given according to user.Require there is stable gps signal to receive to maintain this during work
Item navigation pattern.In this mode of operation, aircraft stabilization last instruction point GPS location, only make pitching and
Rolling instruction (or activation destination pattern), GPS location can be just updated.Under the navigation pattern, according to being supplied to system
Instruction, client, which can change, to arrive：MAG, INS, HM and WP pattern.
4) WP destinations
The navigation pattern is also self-driving pattern, because aircraft can be according to the instruction repertoire for setting and uploading in destination path
Perform different tasks.Require there is stable gps signal to receive to maintain this navigation pattern during work.When the navigation pattern quilt
After activation, user is unable to the direction of change of flight, and the control of camera can be realized in itself by aircraft, or user can be
It is first good defined in destination path before flight.
After activating the navigation pattern, aircraft can fly to next destination according to instruction repertoire from current location, on this road
If barrier in line, aircraft may be impacted.
5) mono- keys of HM make a return voyage
The navigation pattern is shown when (human hand or automatic activation) auto-returned takeoff point can be performed in aircraft, is worked
Shi Yaoqiu has stable gps signal to receive to maintain this navigation pattern.The activation of the navigation pattern has three kinds of modes：
Manually：User is maked a return voyage by designated command aircraft.
Automatic 1：When remote-control communication is interrupted in md4 series aircraft course of normal operation, aircraft can be automatically into certainly
It is dynamic to make a return voyage.
Automatic 2：, can be according to the action of different parameter setting aircraft execution under destination navigation pattern.
After the pattern is activated, aircraft can adjust its postbrachium alignment takeoff point (acquiescence), be increased to safe height
(acquiescence 30m) or present level (if present level is more than 30m) is kept, then back flown according to the cruising speed of 5m/s,
Until reaching takeoff point.
When gui interface shows current location and the direction of aircraft in 2D grating maps, can point out to fly using icon
The direction of row device, and forearm positions are indicated with red.2D grating maps are defaulted as takeoff point with red spots, and just
Overlay mark north N, heading is represented with red arrow, and foundation is oriented to the forearm of aircraft.
The use of GUI one of them most important variable observed is exactly GPS accuracy and satellite connection number, both are in F areas
In show：GPS accuracy is shown in the lower section in F areas, such as shows 4.5m, that is, represents GPS accuracy<4.5m, this is md4 series flights
The standard value of device work, it is good that green satellite icon represents GPS accuracy, when real-time precision may as low as alarm levels when,
Satellite mapping target color can become light blue.When display purple background yellow satellite icon, represent that aircraft loses gps signal
Alarm state, when aircraft is not received by GPS information, or the information received is not suitable for navigating, and satellite icon becomes
Into black, background is red, and satellite connection number shows NA, represents unavailable, and precision shows X.Xm, represents GPS accuracy>8.0m.
Aircraft is positioned without reference to point, therefore can be affected by wind, when not having gps signal, it is impossible to maked a return voyage using a key.
Wireless control signal is a fundamental for ensureing the running of md4 aircraft securities, and institute is corresponded to bar chart in G areas
The percentage of received signal strength, aircraft do not receive remote signal, and remote controler, which can sound the alarm, reminds user.
User can edit the setting of remote controler by the GUI of digital remote control, set interface to have tri- menus of A, B, C,
Menu A includes the basic configuration that user can change, and menu B is used for 7Pin mouthfuls of functions of configuration receiver, and menu C is used to configure
FNC information.The setting interface of remote controler can be activated using the keyboard of remote controler, the selection function that interface is set is enabled, by once
MENU buttons, acquiescence into remote controler setting interface menu A --- RF module options, are moved between setting option, can make
With UP or DOWN arrows, the setting option to be changed is moved to, changes number of its numerical value to before setting using left or right arrow
Value.Confirm the setting of a change, press a MENU key.
The channel of remote controller transmitter, can be simply modified using gui interface.For safe and simple reason, with
And avoiding occurring any problem in operation, the module in aircraft can be realized by remote controler automatic matching function matches somebody with somebody automatically
Put.
The calibration module of remote controler rod volume is set in remote controler, is handled during using remote controler, in remote controler rod volume
The situation that heart point shifts.Need detection rocking bar rod volume whether normal before aircraft takeoff, recall remote configuration interface, it is left
Side information contains the channel value of nine passages of remote controler, Aircam companies logo and current version of firmware number.Keeping being remotely controlled
When device rocking bar is in central point, if the channel value of 1-4 passages is not 0, remote controler rocking bar rod volume central point has occurred and that partially
Move, need to calibrate remote controler rocking bar rod volume at this time.
The remote control command that remote controler is sent is received and processed by unmanned plane receiver, and unmanned plane receives implement body rate-determining steps
It is as follows：
1st, hardware initialization：The peripheral hardwares such as GPIO, interruption, serial ports, USB are initialized.
2nd, module configures：RF communication modules are initialized, the parameter such as configurating channel number, speed, transmission power.Needing
Enter pairing mode when matching, receive the configuration information and configuration module again of remote controller transmitter.
3rd, processing aircraft downlink information is received：The DownLink information passed down by serial ports reception aircraft, obtains
Longitude and latitude, height, etc. winged control parameter.
4th, the control frame of receiver/transmitter：The remote information frame transmitted from encoding board is received by RF modules, is obtained
The rod volume information of each rocking bar, button.
5th, descending chain circuit frame is sent to transmitter：Effective DownLink information is extracted, FMC information frames is packaged into, passes through
RF modules descend into remote controler.
6th, PPM signal is produced：The PPM of each passage is produced according to the rod volume information configuration timer of each rocking bar, button
Waveform.
7th, configuration information is received：The configuration information issued from PC is received by USB, if configuration does not change, return connects
Processing aircraft downlink information is received, if configuration change, the parameters such as channel number, speed are reconfigured by configuration module, so
After return again to reception processing aircraft downlink information.
Receiver configuration 900MHz data radio stations realize data transfer, receive the downlink data of processing aircraft, LED is shown
Receive remote signal and receive the state of aircraft data, produce the PPM signal of each 9 passage of two-way, wherein being used to control all the way
Aircraft, another way are used to control brushless holder and camera.
The communication configuration of receiver end is realized automatically using the matching function of remote controler, and some of remote controller transmitter set
Put, such as channel, can be simply modified using gui interface, without being realized by software RCConfig.
For safe and simple reason, and avoid occurring any problem in operation, the module in aircraft can be by distant
Control device automatic matching function, which is realized, to be automatically configured.Concrete operations mode is：By microwave box installation aboard, oneself on box is pinned
Dynamic pairing button powers on, and is unclamped after waiting 3S.The cursor for setting interface A menu is moved to by remote controler end " pairing " item, press
Right button, " pairing " item are changed into " Waiting " by " IDLE ", choose and press " MENU " key after " Waiting " and confirmed, at this time
Remote controler enters with receiver automatically configures flow, waits 30S or so, and remote controler automatic matching is completed, configuration interface " pairing "
Item shows " OK ", and automatic matching flow terminates at this time, and remote controler main interface receives the Downlink information of aircraft.Need to note
Meaning, synchronization can only have a set of remote controler to be configured with receiver.
Although an embodiment of the present invention has been shown and described, it will be understood by those of ordinary skill in the art that：Not
In the case of departing from the principle of the present invention and objective a variety of change, modification, replacement and modification can be carried out to these embodiments, this
The scope of invention is limited by claim and its equivalent substitution, without creative work improvements introduced etc., should all be included
Within protection scope of the present invention.
Claims (5)
1. a kind of unmanned controller, including remote controler housing and control unit in remote controler housing, data radio station,
It is characterized in that, the positive center section of the remote controler housing sets display screen, in display screen both sides, difference Setting pattern turns
Slide bar, throttle slide bar are changed, button keyboard is set in the downside of display screen, remote controler housing is also in the upper left side of display screen, upper right
Side is respectively arranged to receive the antennal interface, the shutter release taken pictures that send control data, and throttle joystick is neighbouring described
Pattern conversion slide bar is set, and posture control stick is set adjacent to the throttle slide bar, and charging is provided with front side of remote controler housing
Interface, power switch.
2. unmanned controller according to claim 1, it is characterised in that be additionally provided with buzzing on front side of remote controler housing
Device.
3. unmanned controller according to claim 2, it is characterised in that remote controler housing the upper left corner set coach-
Student's switch, the upper right corner set destination to switch, and set the first control passage/second to control in the lower-left of remote controler housing or lower right
Passage switching switch processed.
4. unmanned controller according to claim 3, it is characterised in that corner protector is set in the corner of remote controler housing.
5. the display methods of unmanned controller according to claim 1, data radio station receives aircraft section downlink data,
Export next Flight Condition Data is sent back from aircraft to the display screen of remote controler, correspondingly shown by display screen,
It is characterized in that：Lattice point map P areas are set in the display interface central region of rectangular display screen, aircraft side is shown in P areas
The forearm of position and aircraft is directed toward, and sets multiple rectangles for showing aircraft state information to show around lattice point map area
Frame, the multiple rectangle display box order include：Height A areas, navigation Mode B area, landing secondary status D areas, number of satellite F
Area, signal strength show G areas, battery status H areas, flight time J area, position coordinates M areas；The navigation Mode B area is at least wrapped
Include following navigation pattern：INS inertial navigation systems, MAG magnetometers, GNSS Global Navigation Satellite System, WP destinations, mono- keys of HM return
Boat.
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| CN201711214504.3A CN107945481A (en) | 2017-11-28 | 2017-11-28 | Unmanned controller and its display methods |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110930670A (en) * | 2019-10-17 | 2020-03-27 | 东华理工大学长江学院 | Data processing system for unmanned aerial vehicle surveying and mapping |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1424851A (en) * | 2002-12-30 | 2003-06-18 | 南京熊猫电子股份有限公司 | Miniaturized installation method and device for TV remote controller |
| CN1540287A (en) * | 2003-04-21 | 2004-10-27 | 三星电子株式会社 | Wireless remote controller with guide function and method for providing such function therefor |
| CN105045283A (en) * | 2015-08-19 | 2015-11-11 | 无锡觅睿恪科技有限公司 | Control unit of unmanned plane and operation interface thereof |
| CN105575095A (en) * | 2016-02-03 | 2016-05-11 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle dual-remote-control system |
| CN105912288A (en) * | 2016-04-12 | 2016-08-31 | 上海易天无人飞行器科技有限公司 | Method and system for comprehensive processing display capable of monitoring flight state of unmanned aerial vehicle |
| CN205541399U (en) * | 2016-04-15 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Remote controller |
| CN205692364U (en) * | 2016-06-06 | 2016-11-16 | 天津中翔腾航科技股份有限公司 | A kind of unmanned controller |
| CN205692051U (en) * | 2016-06-06 | 2016-11-16 | 天津中翔腾航科技股份有限公司 | A kind of Portable unmanned machine earth station of integrated remote control |
| CN206147927U (en) * | 2016-10-19 | 2017-05-03 | 厦门汉航精密科技有限公司 | Unmanned aerial vehicle's remote controller structure |
-
2017
- 2017-11-28 CN CN201711214504.3A patent/CN107945481A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1424851A (en) * | 2002-12-30 | 2003-06-18 | 南京熊猫电子股份有限公司 | Miniaturized installation method and device for TV remote controller |
| CN1540287A (en) * | 2003-04-21 | 2004-10-27 | 三星电子株式会社 | Wireless remote controller with guide function and method for providing such function therefor |
| CN105045283A (en) * | 2015-08-19 | 2015-11-11 | 无锡觅睿恪科技有限公司 | Control unit of unmanned plane and operation interface thereof |
| CN105575095A (en) * | 2016-02-03 | 2016-05-11 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle dual-remote-control system |
| CN105912288A (en) * | 2016-04-12 | 2016-08-31 | 上海易天无人飞行器科技有限公司 | Method and system for comprehensive processing display capable of monitoring flight state of unmanned aerial vehicle |
| CN205541399U (en) * | 2016-04-15 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Remote controller |
| CN205692364U (en) * | 2016-06-06 | 2016-11-16 | 天津中翔腾航科技股份有限公司 | A kind of unmanned controller |
| CN205692051U (en) * | 2016-06-06 | 2016-11-16 | 天津中翔腾航科技股份有限公司 | A kind of Portable unmanned machine earth station of integrated remote control |
| CN206147927U (en) * | 2016-10-19 | 2017-05-03 | 厦门汉航精密科技有限公司 | Unmanned aerial vehicle's remote controller structure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110930670A (en) * | 2019-10-17 | 2020-03-27 | 东华理工大学长江学院 | Data processing system for unmanned aerial vehicle surveying and mapping |
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Address after: 528305 No.7 No.2 Jianye Middle Road, Ronggui Science and Technology Industrial Park, Shunde District, Foshan City, Guangdong Province Applicant after: Magnesium Kezhongsi Technology (Foshan) Co.,Ltd. Address before: 528305 No.7 No.2 Jianye Middle Road, Ronggui Science and Technology Industrial Park, Shunde District, Foshan City, Guangdong Province Applicant before: Foshan Anlcom Technology Co.,Ltd. Address after: 528305 No.7 No.2 Jianye Middle Road, Ronggui Science and Technology Industrial Park, Shunde District, Foshan City, Guangdong Province Applicant after: Foshan Anlcom Technology Co.,Ltd. Address before: 528305 No.7 No.2 Jianye Middle Road, Ronggui Science and Technology Industrial Park, Shunde District, Foshan City, Guangdong Province Applicant before: FOSHAN AIRCAM UAV TECHNOLOGY Corp. |
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