CN206224243U - A kind of key landing control system of unmanned plane one - Google Patents
A kind of key landing control system of unmanned plane one Download PDFInfo
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- CN206224243U CN206224243U CN201621147078.7U CN201621147078U CN206224243U CN 206224243 U CN206224243 U CN 206224243U CN 201621147078 U CN201621147078 U CN 201621147078U CN 206224243 U CN206224243 U CN 206224243U
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Abstract
The utility model discloses a kind of key landing control system of unmanned plane one, it is related to unmanned air vehicle technique field, including ground control terminal, radiofrequency launcher, radio-frequency transmitter, flight control system and data acquisition module, the utility model sets take off height, speed etc. by ground control terminal, and data are sent to winged control by ground by radio frequency after pressing the button that takes off, winged control reads current attitude on the ground after being connected to data, judge current flight device on the ground whether level, and aircraft adjusts current pose before take-off, it is ensured that will not be turned on one's side after taking off.And gps data is constantly read in take-off process, it is ensured that aircraft keeps horizontal level to take off in take-off process.The data of data collecting module collected can also be easy to ground control terminal to understand the real-time flight state of aircraft by the radiofrequency launcher two that is connected with flight control system to the transmission of radio-frequency transmitter two with ground control terminal.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, and in particular to a kind of key landing control system of unmanned plane one.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+sector application is the real firm need of unmanned plane；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation,
Disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture wave
The application in unrestrained etc. field, has greatly expanded unmanned plane purposes in itself, developed country also actively extension sector application with
Development unmanned air vehicle technique.
From the point of view of various countries' unmanned plane accident statistics situation, most of accident is occurred during the landing of unmanned plane.
It is substantially on the market at present and takes off manually, and takes off and will turn on one's side in the case of the injustice of ground, it is very unstable, it is necessary to grasp
Make the consummate operation skill of personnel, for new hand, hence it is evident that there is operational not convenient property.
Utility model content
The purpose of this utility model is to provide a kind of key landing control system of unmanned plane one, to solve to lead in the prior art
The drawbacks described above of cause.
A kind of key landing control system of unmanned plane one, including ground control terminal, radiofrequency launcher, radio-frequency transmitter, fly
Control system and data acquisition module, be built-in with parameter setting module on the ground control terminal, take off button and landing button,
In the parameter setting module set parameter include take off height and takeoff speed, the radiofrequency launcher include respectively with ground
Face control terminal and flight control system connection radiofrequency launcher one and radiofrequency launcher two, the radio-frequency transmitter include respectively with
Ground control terminal and the radio-frequency transmitter one and radio-frequency transmitter two of flight control system connection, radiofrequency launcher one and radio frequency reception
The wireless connection of machine one, radiofrequency launcher two and the wireless connection of radio-frequency transmitter two, the data acquisition module include inertia measurement
Unit, GPS, pitot meter and radio altimeter, data acquisition module are connected with flight control system.
Preferably, the ground control terminal is specially mobile phone or panel computer.
Preferably, alarm unit is provided with the ground control terminal, and is connected with ground control terminal.
Preferably, the alarm unit includes buzzer and stroboscopic lamp.
Preferably, the data acquisition module also includes gyroscope, accelerometer, baroceptor and temperature sensor.
Preferably, the flight control system is also associated with electro-heat equipment, and the electro-heat equipment is arranged in unmanned plane main body.
The utility model has the advantage of：Key takeoff control system of the present utility model passes through ground control terminal (hand
Machine or panel computer) set and take off height, speed etc., and ground is pressed after the button that takes off by data by radio frequency transmission
To winged control, winged control is connected to after data reads current attitude on the ground, judge current flight device on the ground whether level, and
And aircraft adjusts current pose before take-off, it is ensured that will not be turned on one's side after taking off.And GPS numbers are constantly read in take-off process
According to, it is ensured that aircraft keeps horizontal level to take off in take-off process.One key is lowered through ground control terminal (mobile phone or electricity
Brain) after triggering landing button, the radio-frequency transmitter flown in control is issued by radiofrequency launcher, and pass through again after parsing data
The data of GPS show that relative altitude judges current how far from the ground, then are slowly landed by flight control system control aircraft.Data are adopted
The data of collection module collection can also be connect by the radiofrequency launcher two being connected with flight control system to the radio frequency with ground control terminal
Receipts machine two sends, and is easy to ground control terminal to understand the real-time flight state of aircraft.
Brief description of the drawings
Fig. 1 is a kind of theory diagram of the key landing control system of unmanned plane described in the utility model.
Fig. 2 is the principle frame of data acquisition module in a kind of key landing control system of unmanned plane described in the utility model
Figure.
Fig. 3 is a kind of take-off process flow chart of the key landing control system of unmanned plane described in the utility model.
Fig. 4 is a kind of decline process flow diagram flow chart of the key landing control system of unmanned plane described in the utility model.
Specific embodiment
For technological means, creation characteristic, reached purpose and effect for realizing the utility model are easy to understand, below
With reference to specific embodiment, the utility model is expanded on further.
As shown in Figures 1 to 4, the key landing control system of a kind of unmanned plane one, including ground control terminal, radio-frequency transmissions
Device, radio-frequency transmitter, flight control system and data acquisition module, are built-in with parameter setting module, rise on the ground control terminal
Fly button and landing button, the parameter set in the parameter setting module includes take off height and takeoff speed, the radio frequency
Transmitter includes the radiofrequency launcher one and radiofrequency launcher two that are connected with ground control terminal and flight control system respectively, described to penetrate
Frequency receiver includes the radio-frequency transmitter one and radio-frequency transmitter two that are connected with ground control terminal and flight control system respectively, radio frequency
Transmitter one and the wireless connection of radio-frequency transmitter one, radiofrequency launcher two and the wireless connection of radio-frequency transmitter two, the data are adopted
Collection module includes Inertial Measurement Unit, GPS, pitot meter and radio altimeter, and data acquisition module is connected with flight control system.
In the utility model, the ground control terminal is specially mobile phone or panel computer, is easy to carry, can be various multiple
Heterocycle is used under border.
In the present embodiment, alarm unit is provided with the ground control terminal, and is connected with ground control terminal, institute
Stating alarm unit includes buzzer and stroboscopic lamp, and when the flying height and speed of unmanned plane exceed warning value, ground control is eventually
Hold and send signal to alarm unit, and start buzzer and stroboscopic lamp, remind operating personnel to note.
In the utility model, the data acquisition module also includes that gyroscope, accelerometer, baroceptor and temperature are passed
Sensor, can be used to gather flight attitude data, acceleration magnitude, ambient pressure and the temperature conditions of unmanned plane, and these information are through flying
Control system is sent to ground control terminal so that operating personnel can according to circumstances adjust the state of flight of unmanned plane.
Additionally, the flight control system is also associated with electro-heat equipment, this kind of electro-heat equipment can be electrothermal tube or heating wire or electricity
Thermolamp pipe etc., the electro-heat equipment is arranged in unmanned plane main body, in night flying, can be timely by thermal imaging detection means
It was found that the orientation residing for flight.
Based on above-mentioned, key takeoff control system of the present utility model is by ground control terminal (mobile phone or flat board electricity
Brain) set and take off height, speed etc., and data are sent to winged control by ground by radio frequency after pressing the button that takes off, and fly to control
Be connected to after data and read current attitude on the ground, judge current flight device on the ground whether level, and before take-off
Aircraft adjusts current pose, it is ensured that will not be turned on one's side after taking off.And gps data is constantly read in take-off process, it is ensured that
Aircraft keeps horizontal level to take off in take-off process.One key is lowered through ground control terminal (mobile phone or computer) triggering drop
Fall after button, the radio-frequency transmitter flown in control is issued by radiofrequency launcher, and parse after data again by the data of GPS
Show that relative altitude judges current how far from the ground, then slowly landed by flight control system control aircraft.Data acquisition module is adopted
The data of collection can also be by the radiofrequency launcher two that is connected with flight control system to the hair of radio-frequency transmitter two with ground control terminal
Send, be easy to ground control terminal to understand the real-time flight state of aircraft.
As known by the technical knowledge, the utility model can be by other essence without departing from its spirit or the reality of essential feature
Scheme is applied to realize.Therefore, embodiment disclosed above, for each side, is all merely illustrative, and is not only
's.It is all in the range of the utility model or in the change being equal in the range of the utility model by the utility model bag
Contain.
Claims (6)
1. the key landing control system of a kind of unmanned plane one, it is characterised in that including ground control terminal, radiofrequency launcher, radio frequency
Receiver, flight control system and data acquisition module, be built-in with parameter setting module on the ground control terminal, take off button and
Landing button, the parameter set in the parameter setting module includes take off height and takeoff speed, the radiofrequency launcher bag
Include the radiofrequency launcher one and radiofrequency launcher two being connected with ground control terminal and flight control system respectively, the radio-frequency transmitter
Including the radio-frequency transmitter one and radio-frequency transmitter two that are connected with ground control terminal and flight control system respectively, radiofrequency launcher one
With the wireless connection of radio-frequency transmitter one, radiofrequency launcher two and the wireless connection of radio-frequency transmitter two, the data acquisition module bag
Inertial Measurement Unit, GPS, pitot meter and radio altimeter are included, data acquisition module is connected with flight control system.
2. the key landing control system of a kind of unmanned plane according to claim 1, it is characterised in that：The ground control is eventually
End is specially mobile phone or panel computer.
3. the key landing control system of a kind of unmanned plane according to claim 1, it is characterised in that：The ground control is eventually
Alarm unit is provided with end, and is connected with ground control terminal.
4. the key landing control system of a kind of unmanned plane according to claim 3, it is characterised in that：The alarm unit bag
Include buzzer and stroboscopic lamp.
5. the key landing control system of a kind of unmanned plane according to claim 4, it is characterised in that：The data acquisition module
Block also includes gyroscope, accelerometer, baroceptor and temperature sensor.
6. the key landing control system of a kind of unmanned plane according to claim 5, it is characterised in that：The flight control system is also
Electro-heat equipment is connected with, the electro-heat equipment is arranged in unmanned plane main body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621147078.7U CN206224243U (en) | 2016-10-21 | 2016-10-21 | A kind of key landing control system of unmanned plane one |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621147078.7U CN206224243U (en) | 2016-10-21 | 2016-10-21 | A kind of key landing control system of unmanned plane one |
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| Publication Number | Publication Date |
|---|---|
| CN206224243U true CN206224243U (en) | 2017-06-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621147078.7U Active CN206224243U (en) | 2016-10-21 | 2016-10-21 | A kind of key landing control system of unmanned plane one |
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| CN (1) | CN206224243U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107515615A (en) * | 2017-08-30 | 2017-12-26 | 泸州深远世宁无人机科技有限公司 | For the landing-gear of unmanned plane in particular circumstances |
| CN112093034A (en) * | 2020-09-22 | 2020-12-18 | 青海奥珞威信息科技有限公司 | Rotor magnetomotive unmanned aerial vehicle undercarriage retraction system |
-
2016
- 2016-10-21 CN CN201621147078.7U patent/CN206224243U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107515615A (en) * | 2017-08-30 | 2017-12-26 | 泸州深远世宁无人机科技有限公司 | For the landing-gear of unmanned plane in particular circumstances |
| CN112093034A (en) * | 2020-09-22 | 2020-12-18 | 青海奥珞威信息科技有限公司 | Rotor magnetomotive unmanned aerial vehicle undercarriage retraction system |
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