CN105320145A - Automatic pilot arranged on fixed-wing unmanned aerial vehicle - Google Patents
Automatic pilot arranged on fixed-wing unmanned aerial vehicle Download PDFInfo
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- CN105320145A CN105320145A CN201510834632.2A CN201510834632A CN105320145A CN 105320145 A CN105320145 A CN 105320145A CN 201510834632 A CN201510834632 A CN 201510834632A CN 105320145 A CN105320145 A CN 105320145A
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Abstract
The invention discloses an automatic pilot arranged on a fixed-wing unmanned aerial vehicle. The automatic pilot arranged on the fixed-wing unmanned aerial vehicle includes a core circuit board and is characterized in that: the core circuit board is provided with a central processing unit, a six-axis gyroscope, an air pressure gage, an air speedometer, and a remote control receiver, wherein the central processing unit is connected to the six-axis gyroscope, the air pressure gage, the air speedometer, and the remote control receiver. The automatic pilot arranged on the fixed-wing unmanned aerial vehicle is suitable for a sensing and mapping unmanned aerial vehicle.
Description
Technical field
The invention belongs to the robot pilot that a kind of unmanned plane uses, particularly a kind of robot pilot be arranged on mapping fixed-wing unmanned plane.
Background technology
Existing mapping fixed-wing unmanned plane robot pilot function is simple, is suitable for the type installed single, generally can only be arranged on a kind of mapping fixed-wing unmanned plane.Other mapping fixed-wing unmanned planes are difficult to adapt to.Namely allow to be installed on other mapping fixed-wing unmanned plane, also having to pass through complicated debugging could use.
In addition, existing robot pilot is difficult to adapt to complicated field condition, often causes mapping fixed-wing unmanned plane to obtain data and does not reach desirable effect.Cause repeatedly repeated work, work efficiency is low, loses time.
Summary of the invention
The object of the invention is to design a kind of mapping fixed-wing unmanned plane robot pilot.
The present invention is to solve existing mapping fixed-wing unmanned plane robot pilot function is simple, be suitable for the type installed single, be difficult to adapt to complicated field condition, obtain the problem that data do not reach desirable effect etc.
For realizing object of the present invention, the technical solution used in the present invention is:
Robot pilot on fixed-wing unmanned plane of the present invention comprises: core circuit plate, and described core circuit plate is provided with central processing unit, six axle gyroscopes, barometer, pitot meter and remote control receiver; Described central processing unit is connected with six axle gyroscopes, barometer, pitot meter and remote control receiver.
The function of described central processing unit is: the signal after reception, process and output processing, for robot pilot work;
The described gyrostatic function of six axles is: obtain attitude information and send central processing unit to, export to aviation mechanism, to ensure this unmanned plane smooth flight after process;
Described barometrical function is: obtain atmospheric pressure elevation information and send central processing unit to, export to aviation mechanism, control unmanned plane during flying height after process;
The function of described integrated pitot meter is: the aerial effective wind speed information that integrated pitot meter obtains is sent to central processing unit, exports to aviation mechanism, make flight more stable after process, increases the stability of unmanned plane aloft airline operation;
The function of described remote control receiver is: send surface instruction in real time to robot pilot, control the flight path of unmanned plane.
Described central processing unit is provided with multiple input interface, multiple output interface and a USB interface.
The invention has the beneficial effects as follows: mapping fixed-wing unmanned plane robot pilot reasonable in design of the present invention, can be installed on multiple mapping fixed-wing unmanned plane, and without the need to debugging.Be provided with unmanned plane of the present invention and adapt to complicated field condition, it can regulate flight attitude automatically according to six axle gyroscopes, automatically regulates flying height, automatically regulates the speed of flight according to pitot meter, thus obtain high-quality surveying and mapping data according to barometer.And it also with the ground signal received according to remote control receiver, will carry out working flight.
Accompanying drawing explanation
Fig. 1 is core circuit plate schematic diagram of the present invention.
Fig. 2 is that parts of the present invention connect block diagram.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described further.
As shown in the figure, the robot pilot on a kind of fixed-wing unmanned plane, comprises core circuit plate, and described core circuit plate is provided with central processing unit, six axle gyroscopes, barometer, pitot meter and remote control receiver; Described central processing unit is connected with six axle gyroscopes, barometer, pitot meter and remote control receiver.
The function of described central processing unit is: the signal after reception, process and output processing, for robot pilot work;
The described gyrostatic function of six axles is: obtain attitude information and send central processing unit to, export to aviation mechanism, to ensure this unmanned plane smooth flight after process;
Described barometrical function is: obtain atmospheric pressure elevation information and send central processing unit to, export to aviation mechanism, control unmanned plane during flying height after process;
The function of described integrated pitot meter is: the aerial effective wind speed information that integrated pitot meter obtains is sent to central processing unit, exports to aviation mechanism, make flight more stable after process, increases the stability of unmanned plane aloft airline operation;
The function of described remote control receiver is: send surface instruction in real time to robot pilot, control the flight path of unmanned plane;
Described central processing unit is provided with multiple input interface, multiple output interface and a USB interface.
Claims (2)
1. a fixed-wing unmanned plane robot pilot, comprises core circuit plate, it is characterized in that described core circuit plate is provided with central processing unit, six axle gyroscopes, barometer, pitot meter and remote control receiver; Described central processing unit is connected with six axle gyroscopes, barometer, pitot meter and remote control receiver:
The function of described central processing unit is: the signal after reception, process and output processing,
For robot pilot work;
The described gyrostatic function of six axles is: obtain attitude information and send central processing unit to,
Aviation mechanism is exported to, to ensure this unmanned plane smooth flight after process;
Described barometrical function is: obtain atmospheric pressure elevation information and send central processing unit to, export to aviation mechanism, control unmanned plane during flying height after process;
The function of described integrated pitot meter is: the aerial effective wind speed information that integrated pitot meter obtains is sent to central processing unit, exports to aviation mechanism, make flight more stable after process, increases the stability of unmanned plane aloft airline operation;
The function of described remote control receiver is: send surface instruction in real time to robot pilot, control the flight path of unmanned plane.
2. fixed-wing unmanned plane robot pilot according to claim 1, is characterized in that described central processing unit is provided with multiple input interface, multiple output interface and a USB interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510834632.2A CN105320145A (en) | 2015-11-25 | 2015-11-25 | Automatic pilot arranged on fixed-wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510834632.2A CN105320145A (en) | 2015-11-25 | 2015-11-25 | Automatic pilot arranged on fixed-wing unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN105320145A true CN105320145A (en) | 2016-02-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510834632.2A Pending CN105320145A (en) | 2015-11-25 | 2015-11-25 | Automatic pilot arranged on fixed-wing unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105843249A (en) * | 2016-03-22 | 2016-08-10 | 安徽大学 | Unmanned aerial vehicle automatic navigation system based on Pixhawk flight control and navigation method thereof |
Citations (4)
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|---|---|---|---|---|
| US20080077284A1 (en) * | 2006-04-19 | 2008-03-27 | Swope John M | System for position and velocity sense of an aircraft |
| CN102431643A (en) * | 2011-11-30 | 2012-05-02 | 中国南方航空工业(集团)有限公司 | Automatic pilot of unmanned plane |
| CN102830708A (en) * | 2012-09-05 | 2012-12-19 | 北京理工大学 | ARM and FPGA (Field Programmable Gate Array) architecture based autopilot of fixed wing unmanned aerial vehicle |
| CN204790578U (en) * | 2015-07-27 | 2015-11-18 | 中恒天信（天津）航空科技有限公司 | General automatic pilot of unmanned vehicles |
-
2015
- 2015-11-25 CN CN201510834632.2A patent/CN105320145A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080077284A1 (en) * | 2006-04-19 | 2008-03-27 | Swope John M | System for position and velocity sense of an aircraft |
| US20110184593A1 (en) * | 2006-04-19 | 2011-07-28 | Swope John M | System for facilitating control of an aircraft |
| CN102431643A (en) * | 2011-11-30 | 2012-05-02 | 中国南方航空工业(集团)有限公司 | Automatic pilot of unmanned plane |
| CN102830708A (en) * | 2012-09-05 | 2012-12-19 | 北京理工大学 | ARM and FPGA (Field Programmable Gate Array) architecture based autopilot of fixed wing unmanned aerial vehicle |
| CN204790578U (en) * | 2015-07-27 | 2015-11-18 | 中恒天信（天津）航空科技有限公司 | General automatic pilot of unmanned vehicles |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105843249A (en) * | 2016-03-22 | 2016-08-10 | 安徽大学 | Unmanned aerial vehicle automatic navigation system based on Pixhawk flight control and navigation method thereof |
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Application publication date: 20160210 |
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