CN204515148U - A kind of integrated navigation is cruised unmanned aerial vehicle - Google Patents
A kind of integrated navigation is cruised unmanned aerial vehicle Download PDFInfo
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- CN204515148U CN204515148U CN201520205264.0U CN201520205264U CN204515148U CN 204515148 U CN204515148 U CN 204515148U CN 201520205264 U CN201520205264 U CN 201520205264U CN 204515148 U CN204515148 U CN 204515148U
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Abstract
The utility model relates to a kind of integrated navigation and to cruise unmanned aerial vehicle, comprising: inertial navigation system, GPS positioning system and processor module; Described inertial navigation system comprises: accelerometer, gyroscope, described accelerometer, gyroscope are connected with corresponding modulate circuit respectively, and the output terminal of each modulate circuit is connected with processor module by two path analoging switch, A/D module, the described control end of two path analoging switch is connected with the control output end of processor module; Described GPS positioning system comprises, GPS receiver module, and this GPS receiver module is connected with processor module by serial ports; Described processor module is also connected with the memory module storing the map that cruises; Described integrated navigation cruise unmanned aerial vehicle fuselage on be also provided with touch-screen, this touch-screen is connected with processor module, with input control order; And described processor module is also connected with on-air radio transceiver module, and be connected with ground control station by on-air radio transceiver module.
Description
Technical field
The utility model relates to unmanned aerial vehicle field.
Background technology
The Navigation Control of unmanned aerial vehicle has two kinds of realization means, and one is INS (inertial navigation system), and another kind adopts system GPS(global positioning satellite system); Because INS and GPS has relative merits separately, if therefore adopt a kind of navigate mode separately, then can not effectively carry out high-precision attitude process and navigation in real time for a long time, flight stability and the reliability of unmanned aerial vehicle can not be ensured.
Utility model content
The purpose of this utility model is to provide a kind of integrated navigation and cruises unmanned aerial vehicle, to solve the technical matters of integrated navigation and setting flight path.
In order to solve the problems of the technologies described above, the utility model provides a kind of integrated navigation and to cruise unmanned aerial vehicle, comprising: inertial navigation system, GPS positioning system and processor module; Described inertial navigation system comprises: accelerometer, gyroscope, described accelerometer, gyroscope are connected with corresponding modulate circuit respectively, and the output terminal of each modulate circuit is connected with processor module by two path analoging switch, A/D module, the described control end of two path analoging switch is connected with the control output end of processor module; Described GPS positioning system comprises, GPS receiver module, and this GPS receiver module is connected with processor module by serial ports; Described processor module is also connected with the memory module storing the map that cruises; Described integrated navigation cruise unmanned aerial vehicle fuselage on be also provided with touch-screen, this touch-screen is connected with processor module, with input control order; And described processor module is also connected with on-air radio transceiver module, and be connected with ground control station by on-air radio transceiver module.
Further, described processor module is also connected with image collecting device, and is suitable for view data to be stored by memory module, and/or is sent to ground control station by on-air radio transceiver module.
Further, the cruise fuselage of unmanned aerial vehicle of described integrated navigation is coated with photovoltaic panel, and photovoltaic panel is connected by the cruise feed circuit of unmanned aerial vehicle of charge controller and described integrated navigation.
Further, described on-air radio transceiver module comprises: WiFi module and CDMA module, and described WiFi module is connected with processor module respectively with CDMA module.
The beneficial effects of the utility model are, integrated navigation of the present utility model is cruised unmanned aerial vehicle, and its advantage achieved two kinds are navigated by inertial navigation system, GPS positioning system is combined together, improves navigation accuracy, and in conjunction with airborne map, achieve autonomous cruise function; The utility model also can set cruise route by touch-screen and check corresponding data, offers convenience to use.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is that integrated navigation of the present utility model is cruised the theory diagram of unmanned aerial vehicle.
Embodiment
By reference to the accompanying drawings the utility model is described in further detail now.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present utility model are described in a schematic way, and therefore it only shows the formation relevant with the utility model.
As shown in Figure 1, a kind of integrated navigation of the present utility model is cruised unmanned aerial vehicle, comprising: for driving the power system of unmanned aerial vehicle, inertial navigation system, GPS positioning system and processor module; Described inertial navigation system comprises: accelerometer, gyroscope, described accelerometer, gyroscope are connected with corresponding modulate circuit respectively, and the output terminal of each modulate circuit is connected with processor module by two path analoging switch, A/D module, the described control end of two path analoging switch is connected with the control output end of processor module; Described GPS positioning system comprises, GPS receiver module, and this GPS receiver module is connected with processor module by serial ports; Described processor module is also connected with the memory module storing the map that cruises; Described integrated navigation cruise unmanned aerial vehicle fuselage on be also provided with the touch-screen, the voice input module that are connected with processor module, with input control order; And described processor module is also connected with on-air radio transceiver module, and be connected with ground control station by on-air radio transceiver module.
This integrated navigation unmanned aerial vehicle that cruises overcomes INS and easily produces offset error, and error infinitely becomes large defect, also overcome GPS output speed slow, and due to weather, the defect that the intermittent signal that the reasons such as position cause is lost, both advantages are merged, ensure that unmanned aerial vehicle autonomous cruise; And directly can set flight path to unmanned plane by touch-screen and the memory module storing the map that cruises.
Described processor module is also connected with image collecting device, and is suitable for view data to be stored by memory module, and/or is sent to ground control station by on-air radio transceiver module, to realize the acquisition function of unmanned aerial vehicle to ground data.
The cruise fuselage of unmanned aerial vehicle of described integrated navigation is coated with photovoltaic panel, and photovoltaic panel is connected by the cruise feed circuit of unmanned aerial vehicle of charge controller and described integrated navigation, to improve the cruising ability of unmanned aerial vehicle further.
Described on-air radio transceiver module comprises: the 2G module (or 3G or 4G module), WiFi module and the CDMA module that are connected with processor module; Make aircraft can receive multiple wireless signal, improve controlled in wireless, or the versatility of Signal transmissions.
Described processor module is such as but not limited to employing S3C2440 embedded chip.The power system of described unmanned aerial vehicle, inertial navigation system, GPS positioning system and processor module adopt hydrogen fuel cell as power supply.
The wing of unmanned aerial vehicle is provided with thin-film solar cells, and thin-film solar cells is used for powering to the power system of described unmanned aerial vehicle.
With above-mentioned according to desirable embodiment of the present utility model for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this utility model technological thought, can carry out various change and amendment completely.The technical scope of this utility model is not limited to the content on instructions, must determine its technical scope according to right.
Claims (2)
1. integrated navigation is cruised a unmanned aerial vehicle, it is characterized in that, comprising:
Inertial navigation system, GPS positioning system and processor module;
Described inertial navigation system comprises: accelerometer, gyroscope, described accelerometer, gyroscope are connected with corresponding modulate circuit respectively, and the output terminal of each modulate circuit is connected with processor module by two path analoging switch, A/D module, the described control end of two path analoging switch is connected with the control output end of processor module;
Described GPS positioning system comprises, GPS receiver module, and this GPS receiver module is connected with processor module by serial ports;
Described processor module is also connected with the memory module storing the map that cruises;
Described integrated navigation cruise unmanned aerial vehicle fuselage on be also provided with touch-screen, this touch-screen is connected with processor module, with input control order;
And described processor module is also connected with on-air radio transceiver module, and be connected with ground control station by on-air radio transceiver module.
2. integrated navigation as claimed in claim 1 is cruised unmanned aerial vehicle, it is characterized in that, described processor module is also connected with image collecting device, and is suitable for view data to be stored by memory module, and/or is sent to ground control station by on-air radio transceiver module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520205264.0U CN204515148U (en) | 2015-04-07 | 2015-04-07 | A kind of integrated navigation is cruised unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520205264.0U CN204515148U (en) | 2015-04-07 | 2015-04-07 | A kind of integrated navigation is cruised unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN204515148U true CN204515148U (en) | 2015-07-29 |
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| CN201520205264.0U Expired - Fee Related CN204515148U (en) | 2015-04-07 | 2015-04-07 | A kind of integrated navigation is cruised unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105334861A (en) * | 2015-10-18 | 2016-02-17 | 上海圣尧智能科技有限公司 | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane |
-
2015
- 2015-04-07 CN CN201520205264.0U patent/CN204515148U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105334861A (en) * | 2015-10-18 | 2016-02-17 | 上海圣尧智能科技有限公司 | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane |
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| 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: 20150729 Termination date: 20160407 |
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| CF01 | Termination of patent right due to non-payment of annual fee |