CN205861063U - A kind of model plane fly automatically with seeking track navigation system - Google Patents
A kind of model plane fly automatically with seeking track navigation system Download PDFInfo
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- CN205861063U CN205861063U CN201620776754.0U CN201620776754U CN205861063U CN 205861063 U CN205861063 U CN 205861063U CN 201620776754 U CN201620776754 U CN 201620776754U CN 205861063 U CN205861063 U CN 205861063U
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- navigation system
- model plane
- controller
- fly
- communicator
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Abstract
nullThis utility model relates to a kind of model plane and automatically flies with seeking track navigation system，Including the control system for being arranged on model plane、Navigation elements、Video camera and remote control terminal，Control system includes controller、Communicator and motor driver，Video camera、Communicator and motor driver are connected with controller respectively，Navigation elements includes GPS sensor、Galileo navigation system、Triones navigation system is or/and GLONASS navigation system，Navigation elements is connected by transducer with controller，Wireless communicator it is provided with in remote control terminal、Display screen、Storage has the memorizer of electronic chart、Image processor and remote controllers，Wireless communicator is connected with communicator，Memorizer、Image processor、Display screen and remote controllers are connected with remote controllers respectively，Increase the reliability of navigation system，Reduce the interruption of navigation，By increasing video camera and memorizer、Image processor，Also can provide in properly functioning and seek track data，Avoid aircraft bombing and fly to lose.
Description
Technical field
This utility model relates to the technical field of a kind of navigation system, and especially a kind of model plane fly automatically with seeking track navigation
System.
Background technology
In recent years, the research and development heat of depopulated helicopter has been risen in various countries, and the depopulated helicopter of new research and development competitively goes out in each continent
Existing, and at military affairs, emergency response, monitor, take photo by plane and the aspect such as precision agricultural management plays the part of important function.Many rotors without
Man-machine, construct fairly simple, price also ratio is less expensive, and most important is that it need not emission system, moreover it is possible to VTOL, to taking off
Environment no requirement (NR), advantage maximum compared with fixed-wing is the most freely to hover, and flight motility is the most superb,
Can use various speed, flies in the air route of various flight profile, mission profiles, thus than fixed-wing unmanned plane difficult of investigation, rescue etc.
In business environment, have more application advantage.
Many rotor wing unmanned aerial vehicles in the market can only use GPS alignment sensor to navigate, when aircraft flies automatically
In have no progeny employing manually flight, but in practical situation, after once gps signal used by flight is lost automatically, remote signal is the most several
Impossible smooth and easy transmission, additionally after gps signal is lost, operator are difficult to judge various terrain data simply by virtue of naked eyes
Realize the flight of unmanned plane or model plane, cause aircraft bombing and fly to lose, causing potential safety hazard.
Therefore, it is necessary to a kind of model plane of design fly with seeking track navigation system automatically, it is achieved when gps signal is lost, behaviour
Make personnel and still can realize the flight of remotely pilotless machine or model plane according to the various terrain datas of systematic analysis.
Utility model content
The purpose of this utility model is to provide a kind of model plane automatically to fly with seeking track navigation system, it is intended to solve existing
In technology, many rotor wing unmanned aerial vehicles in the market can only use GPS alignment sensor to navigate, automatically used by flight
After gps signal is lost, the most hardly possible smooth and easy transmission of remote signal, additionally after gps signal is lost, operator are only difficult to
Only judge that various terrain data, to realize the flight of unmanned plane or model plane, causes aircraft bombing and flies to lose, causing safety by naked eyes
The problem of hidden danger.
This utility model is achieved in that a kind of model plane fly with seeking track navigation system, including for being arranged on automatically
Control system, navigation elements, video camera and remote control terminal on model plane, described control system includes controller, communication
Device and motor driver, described video camera, communicator and motor driver be connected with described controller respectively, described navigation
Unit includes that GPS sensor, Galileo navigation system, triones navigation system are or/and GLONASS navigation system, described navigation list
It is connected by transducer between first and described controller, in described remote control terminal, is provided with wireless communicator, display screen, storage
Have the memorizer of electronic chart, image processor and remote controllers, described wireless communicator to be connected with communicator, described in deposit
Reservoir, image processor, display screen and remote controllers are connected with described remote controllers respectively.
Further, described a kind of model plane automatically fly with also include in seeking track navigation system flight attitude derivation device,
Attitude controller, speed control, inertia measurement sensor and baroceptor, described flight attitude derivation device, attitude control
Device processed, speed control, inertia measurement sensor and baroceptor are connected with described controller respectively.
Further, described inertia measurement sensor is provided with three-axis gyroscope, accelerometer and timing correcting device, described
Three-axis gyroscope uses the one in electrostatic gyroscope, laser gyro, optical fibre gyro, micromechanical gyro.
Further, during described remote control terminal is mobile terminal, Intelligent bracelet, joystick and intelligent helmet extremely
Few one.
Further, velocity sensor and acceleration transducer, described acceleration it are provided with in described remote control terminal
Sensor is connected with described remote controllers.
Further, described a kind of model plane automatically fly and also include solar energy signal indicator, earth station with seeking track navigation system
Signal transmitting and receiving unit and remote controller signal receive unit, and described ground station signals Transmit-Receive Unit is with described solar energy signal indicator even
Connecing, described remote controller signal receives unit and is connected with described controller and described wireless communicator respectively, and described solar energy is believed
Number device includes solar panels, charger, lithium battery and framing signal emitter, and described solar panels are electrically connected with described charging
Equipment, described charger is electrically connected with described lithium battery, and described lithium battery is electrically connected with described framing signal emitter, described
Framing signal emitter is connected with described ground station signals Transmit-Receive Unit.
Further, described framing signal emitter uses the discontinuous emitter of 37.5 KHz.
Further, described ground station signals Transmit-Receive Unit is provided with the receptor coordinating described framing signal emitter.
Compared with prior art, a kind of model plane that this utility model provides fly with seeking track navigation system, by setting automatically
Put and include that GPS sensor, Galileo navigation system, triones navigation system are or/and the navigation elements of GLONASS navigation system, control
System processed, video camera and remote control terminal, add the reliability of navigation system, thus decrease the interruption of navigation, logical
Cross to increase video camera and arrange storage at remote control terminal and have the memorizer of electronic chart, image processor, even if occurring
Compeling degradation accident, video camera still can send data to remote control terminal, after picture carries out Treatment Analysis and in storage
Location on device, draws model plane present position after being combined, also can provide and seek track data in properly functioning, it is to avoid fried
The flying of machine and model plane is lost.
Accompanying drawing explanation
Fig. 1 is that a kind of model plane that the present embodiment provides fly automatically with the theory diagram seeking track navigation system.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing and enforcement
Example, is further elaborated to this utility model.Should be appreciated that specific embodiment described herein is only in order to explain
This utility model, is not used to limit this utility model.
Below in conjunction with specific embodiment, realization of the present utility model is described in detail.
With reference to Fig. 1, the preferred embodiment provided for this utility model.
A kind of model plane that the present embodiment provides fly with seeking track navigation system, including for being arranged on model plane automatically
Control system, navigation elements, video camera 5 and remote control terminal, wherein, control system include controller 7, communicator 17 with
And motor driver 8, video camera 5, communicator 17 and motor driver 8 be connected with controller 7 respectively, described navigation elements bag
Include GPS sensor 1, Galileo navigation system 2, triones navigation system 3 or/and GLONASS navigation system 4, described navigation elements
It is connected by transducer 6 with between controller 7, is provided with wireless communicator 11 in remote control terminal, display screen 12, storage have electricity
The memorizer 13 of sub-map, image processor 14 and remote controllers 15, wireless communicator 11 is connected with communicator 17, storage
Device 13, image processor 14, display screen 12 and remote controllers 15 are connected with remote controllers 15 respectively.
Above-mentioned a kind of model plane fly with seeking track navigation system automatically, include that GPS sensor 1, Galileo are led by setting
Boat system 2, triones navigation system 3 are or/and the navigation elements of GLONASS navigation system 4, control system, video camera 5 and remotely
Control terminal, add the reliability of navigation system, thus decrease the interruption of navigation, by increasing video camera 5 and far
Process control terminal arranges storage the memorizer 13 of electronic chart, image processor 14, even if occurring to compel degradation accident, video camera
5 still can send data to remote control terminal, picture is carried out after Treatment Analysis with location on memorizer 13,
Draw model plane present position after being combined, also can provide in properly functioning and seek track data, it is to avoid the flying of aircraft bombing and model plane is lost.
Specifically, above-mentioned a kind of model plane automatically fly with also include in seeking track navigation system flight attitude derivation device,
Attitude controller 7, speed control 7, inertia measurement sensor and baroceptor, described flight attitude derivation device, attitude
Controller 7, speed control 7, inertia measurement sensor and baroceptor are connected with controller 7 respectively, so, and flight attitude
The data of the corresponding detection of derivation device, attitude controller 7, speed control 7, inertia measurement sensor and baroceptor will
Send after processing to controller 7, be transferred to remote control terminal and carry out operating reference.
Further, described inertia measurement sensor is provided with three-axis gyroscope, accelerometer and timing correcting device, described
Three-axis gyroscope uses the one in electrostatic gyroscope, laser gyro, optical fibre gyro, micromechanical gyro.
It addition, in the present embodiment, above-mentioned remote control terminal can be mobile terminal, Intelligent bracelet, joystick
And in intelligent helmet at least one.
In the present embodiment, being provided with velocity sensor and acceleration transducer in above-mentioned remote control terminal, this adds
Velocity sensor is connected with remote controllers 15, so, as long as remote control terminal has the existence of speed or acceleration,
Carry out being sent to controller 7 by remote controllers 15 by this, carry out the control of correspondence.
Further, described a kind of model plane automatically fly and also include solar energy signal indicator 9, ground with seeking track navigation system
Stand signal transmitting and receiving unit 10 and remote controller signal receives unit 16, and wherein, ground station signals Transmit-Receive Unit 10 is with controller 7 even
Connecing, remote controller signal receives unit 16 and is connected with controller 7 and wireless communicator 11 respectively, and described solar energy signal indicator 9 is wrapped
Including solar panels, charger, lithium battery and framing signal emitter, described solar panels embed the end face of model plane, described in fill
Electricity equipment, lithium battery and framing signal emitter package are in same hard metal box, and described solar panels are electrically connected with and fill
Electricity equipment, described charger is electrically connected with lithium battery, and described lithium battery is electrically connected with framing signal emitter, and described location is believed
Number emitter is connected with ground station signals Transmit-Receive Unit 10.
Further, described framing signal emitter uses the discontinuous emitter of 37.5 KHz, and its effect is similar to
Black box, it is simple to reseaching staff seeks track.
Further, described ground station signals Transmit-Receive Unit 10 is provided with the receptor coordinating framing signal emitter, and it is made
With seeking track after being easy for the dropouts such as GPS.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all at this
Any amendment, equivalent and the improvement etc. made within the spirit of utility model and principle, should be included in this utility model
Protection domain within.
Claims (8)
1. model plane fly automatically with seeking track navigation system, it is characterised in that include the control system for being arranged on model plane
System, navigation elements, video camera and remote control terminal, described control system includes that controller, communicator and motor drive
Device, described video camera, communicator and motor driver be connected with described controller respectively, and described navigation elements includes that GPS passes
Sensor, Galileo navigation system, triones navigation system or/and GLONASS navigation system, described navigation elements and described controller
Between connected by transducer, be provided with wireless communicator in described remote control terminal, display screen, storage have depositing of electronic chart
Reservoir, image processor and remote controllers, described wireless communicator is connected with communicator, described memorizer, image procossing
Device, display screen and remote controllers are connected with described remote controllers respectively.
2. a kind of model plane as claimed in claim 1 fly with seeking track navigation system automatically, it is characterised in that described a kind of model plane
Automatically flight also includes flight attitude derivation device, attitude controller, speed control, inertia measurement in seeking track navigation system
Sensor and baroceptor, described flight attitude derivation device, attitude controller, speed control, inertia measurement sensor
It is connected with described controller respectively with baroceptor.
3. a kind of model plane as claimed in claim 2 fly with seeking track navigation system automatically, it is characterised in that described inertia measurement
Sensor is provided with three-axis gyroscope, accelerometer and timing correcting device, and described three-axis gyroscope uses electrostatic gyroscope, laser top
One in spiral shell, optical fibre gyro, micromechanical gyro.
4. a kind of model plane as described in any one of claims 1 to 3 fly with seeking track navigation system automatically, it is characterised in that institute
Stating remote control terminal is at least one in mobile terminal, Intelligent bracelet, joystick and intelligent helmet.
5. a kind of model plane as claimed in claim 4 fly with seeking track navigation system automatically, it is characterised in that described long-range control
Being provided with velocity sensor and acceleration transducer in terminal, described acceleration transducer is connected with described remote controllers.
6. a kind of model plane as claimed in claim 1 fly with seeking track navigation system automatically, it is characterised in that described a kind of model plane
Automatically with seeking track navigation system, flight also includes that solar energy signal indicator, ground station signals Transmit-Receive Unit and remote controller signal receive
Unit, described ground station signals Transmit-Receive Unit is connected with described solar energy signal indicator, and described remote controller signal receives unit respectively
Being connected with described controller and described wireless communicator, described solar energy signal indicator includes solar panels, charger, lithium
Battery and framing signal emitter, described solar panels are electrically connected with described charger, and described charger is electrically connected with institute
Stating lithium battery, described lithium battery is electrically connected with described framing signal emitter, described framing signal emitter and described earth station
Signal transmitting and receiving unit connects.
7. a kind of model plane as claimed in claim 6 fly with seeking track navigation system automatically, it is characterised in that described framing signal
Emitter uses the discontinuous emitter of 37.5 KHz.
8. a kind of model plane as claimed in claim 6 fly with seeking track navigation system automatically, it is characterised in that described earth station believes
Number Transmit-Receive Unit is provided with the receptor coordinating described framing signal emitter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620776754.0U CN205861063U (en) | 2016-07-21 | 2016-07-21 | A kind of model plane fly automatically with seeking track navigation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620776754.0U CN205861063U (en) | 2016-07-21 | 2016-07-21 | A kind of model plane fly automatically with seeking track navigation system |
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| Publication Number | Publication Date |
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| CN205861063U true CN205861063U (en) | 2017-01-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620776754.0U Expired - Fee Related CN205861063U (en) | 2016-07-21 | 2016-07-21 | A kind of model plane fly automatically with seeking track navigation system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606734A (en) * | 2018-11-30 | 2019-04-12 | 中国运载火箭技术研究院 | A kind of master-slave mode space micro air vehicle |
-
2016
- 2016-07-21 CN CN201620776754.0U patent/CN205861063U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606734A (en) * | 2018-11-30 | 2019-04-12 | 中国运载火箭技术研究院 | A kind of master-slave mode space micro air vehicle |
| CN109606734B (en) * | 2018-11-30 | 2021-02-09 | 中国运载火箭技术研究院 | Master-slave type space microminiature aircraft |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170104 Termination date: 20180721 |
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| CF01 | Termination of patent right due to non-payment of annual fee |