CN204937485U - Unmanned aerial vehicle round trip flight control switching system - Google Patents
Unmanned aerial vehicle round trip flight control switching system Download PDFInfo
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- CN204937485U CN204937485U CN201520583212.7U CN201520583212U CN204937485U CN 204937485 U CN204937485 U CN 204937485U CN 201520583212 U CN201520583212 U CN 201520583212U CN 204937485 U CN204937485 U CN 204937485U
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Abstract
The utility model relates to a kind of unmanned aerial vehicle round trip flight control switching system, there is the frame of unmanned plane, described frame comprises fixed-wing and many rotors, described fixed-wing is connected with fixed-wing motor and many rotors motor-driven respectively with many rotors, described fixed-wing motor and many rotors motor are all electrically connected with round trip flight row gesture stability instrument by wire, described round trip flight row gesture stability instrument comprises sensor and control unit, and the mouth of described sensor is connected with the input end of control unit.The utility model can realize the task of large voyage among a small circle; Point-to-point flight can be realized; Vertical takeoff and landing can be realized; Alleviate the requirement to flying hand and place; Fixed-wing fixed point can be realized.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly a kind of unmanned aerial vehicle round trip flight control switching system.
Background technology
Robot airplane is called for short " unmanned plane ", can be divided into: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc. from technical standpoint definition.Unmanned plane, by application, can be divided into military and civilian.Military aspect, unmanned plane is divided into scout and target drone, at present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned plane itself greatly.
But unmanned plane application is at present limited by very large and comprises continuation of the journey, stable, with safety.Fixed-wing has high continuation of the journey, high stability and relative safety, but has lacked the problem of fixed point with low idle job, takes off simultaneously and lands also to flying the very large restriction in hand place.
Summary of the invention
The purpose of this utility model overcomes the defect that prior art exists, and provides a kind of unmanned aerial vehicle round trip flight control switching system of reasonable in design, the task that can realize large voyage among a small circle.
The technical scheme realizing the utility model object is: a kind of unmanned aerial vehicle round trip flight control switching system, there is the frame of unmanned plane, described frame comprises fixed-wing and many rotors, described fixed-wing is connected with fixed-wing motor and many rotors motor-driven respectively with many rotors, described fixed-wing motor and many rotors motor are all electrically connected with round trip flight row gesture stability instrument by wire, described round trip flight row gesture stability instrument comprises sensor and control unit, and the mouth of described sensor is connected with the input end of control unit.
Round trip flight row gesture stability instrument described in technique scheme also has wireless communication module, and described wireless communication module is electrically connected with control unit, and is connected with ground base station wireless telecommunications.
Sensor described in technique scheme comprises geomagnetic sensor, three-axis gyroscope and weight sensor etc.
After adopting technique scheme, the utility model has following positive effect:
(1) the utility model can realize the task of large voyage among a small circle; Point-to-point flight can be realized; Vertical takeoff and landing can be realized; Alleviate the requirement to flying hand and place; Fixed-wing fixed point can be realized.
(2) features such as the utility model has structure simply, reasonable in design, easy to operate.
(3) round trip flight row gesture stability instrument of the present utility model can realize carrying out flight in conjunction with frame and switch fixed-wing and many rotors, realize taking off vertically among a small circle, arrive predetermined altitude and progressively switch to fixed-wing continuation of the journey, arrive intended target task to arrive intended target and progressively switch to many rotors and carry out brake and fixed point task, make a return voyage machine-processed with go to fly identical.
Accompanying drawing explanation
In order to make content of the present utility model more easily be clearly understood, below according to specific embodiment also by reference to the accompanying drawings, the utility model is described in further detail, wherein
Fig. 1 is structural representation of the present utility model;
Attached number in the figure is: frame 1, fixed-wing 2, many rotors 3, fixed-wing motor 4, many rotors motor 5, round trip flight row gesture stability instrument 6, sensor 7, control unit 8, wireless communication module 9, ground base station 10.
Detailed description of the invention
(embodiment 1)
See Fig. 1, the utility model has the frame 1 of unmanned plane, frame 1 comprises fixed-wing 2 and many rotors 3, fixed-wing 2 and many rotors 3 are in transmission connection with fixed-wing motor 4 and many rotors motor 5 respectively, fixed-wing motor 4 and many rotors motor 5 are all electrically connected with round trip flight row gesture stability instrument 6 by wire, round trip flight row gesture stability instrument 6 comprises sensor 7 and control unit 8, and the mouth of sensor 7 is connected with the input end of control unit 8.
Round trip flight row gesture stability instrument 6 also has wireless communication module 9, and wireless communication module 9 is electrically connected with control unit 8, and is connected with ground base station 10 wireless telecommunications.
Sensor 7 comprises geomagnetic sensor, three-axis gyroscope and weight sensor.
Principle of work of the present utility model is: round trip flight row gesture stability instrument 6 can realize carrying out flight in conjunction with frame and switch fixed-wing 2 and many rotors 3, realize taking off vertically among a small circle, arrival predetermined altitude progressively switches to fixed-wing 2 and continues a journey, arrive intended target task to arrive intended target and progressively switch to many rotors 3 and carry out brake and fixed point task, make a return voyage machine-processed with go to fly identical.
Above-described specific embodiment; the purpose of this utility model, technical scheme and beneficial effect are further described; be understood that; the foregoing is only specific embodiment of the utility model; be not limited to the utility model; all within spirit of the present utility model and principle, any amendment made, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (3)
1. a unmanned aerial vehicle round trip flight control switching system, there is the frame (1) of unmanned plane, it is characterized in that: described frame (1) comprises fixed-wing (2) and many rotors (3), described fixed-wing (2) and many rotors (3) are in transmission connection with fixed-wing motor (4) and many rotors motor (5) respectively, described fixed-wing motor (4) and many rotors motor (5) are all electrically connected with round trip flight row gesture stability instrument (6) by wire, described round trip flight row gesture stability instrument (6) comprises sensor (7) and control unit (8), the mouth of described sensor (7) is connected with the input end of control unit (8).
2. unmanned aerial vehicle round trip flight control switching system according to claim 1, it is characterized in that: described round trip flight row gesture stability instrument (6) also has wireless communication module (9), described wireless communication module (9) is electrically connected with control unit (8), and is connected with ground base station (10) wireless telecommunications.
3. unmanned aerial vehicle round trip flight control switching system according to claim 2, is characterized in that: described sensor (7) comprises geomagnetic sensor, three-axis gyroscope and weight sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520583212.7U CN204937485U (en) | 2015-08-06 | 2015-08-06 | Unmanned aerial vehicle round trip flight control switching system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520583212.7U CN204937485U (en) | 2015-08-06 | 2015-08-06 | Unmanned aerial vehicle round trip flight control switching system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937485U true CN204937485U (en) | 2016-01-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520583212.7U Active CN204937485U (en) | 2015-08-06 | 2015-08-06 | Unmanned aerial vehicle round trip flight control switching system |
Country Status (1)
| Country | Link |
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| CN (1) | CN204937485U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108519776A (en) * | 2018-04-04 | 2018-09-11 | 东北大学 | A kind of flight control system based on mobile phone |
| CN111240359A (en) * | 2020-01-17 | 2020-06-05 | 广东汇卓航科技有限公司 | Remote take-off and landing and double-remote control switching control system for unmanned aerial vehicle |
| WO2021035623A1 (en) * | 2019-08-29 | 2021-03-04 | 深圳市大疆创新科技有限公司 | Flight control method and device and aircraft |
-
2015
- 2015-08-06 CN CN201520583212.7U patent/CN204937485U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108519776A (en) * | 2018-04-04 | 2018-09-11 | 东北大学 | A kind of flight control system based on mobile phone |
| CN108519776B (en) * | 2018-04-04 | 2021-06-04 | 东北大学 | Flight control system based on mobile phone |
| WO2021035623A1 (en) * | 2019-08-29 | 2021-03-04 | 深圳市大疆创新科技有限公司 | Flight control method and device and aircraft |
| CN111240359A (en) * | 2020-01-17 | 2020-06-05 | 广东汇卓航科技有限公司 | Remote take-off and landing and double-remote control switching control system for unmanned aerial vehicle |
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