CN205620816U - Unmanned helicopter flight control system - Google Patents
Unmanned helicopter flight control system Download PDFInfo
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- CN205620816U CN205620816U CN201620302568.3U CN201620302568U CN205620816U CN 205620816 U CN205620816 U CN 205620816U CN 201620302568 U CN201620302568 U CN 201620302568U CN 205620816 U CN205620816 U CN 205620816U
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- depopulated helicopter
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Abstract
The utility model provides an unmanned helicopter flight control system, which comprises a power supply module, power module with fly to control chip module and connect, fly to control chip module's input and GPS module, pneumatics meter module, the magnetic sensor module, inertia measured module's output connection, the output connection of the remote controller on remote control receiver and ground is passed through in the input that flies to control chip module, the remote controller passes through radio wave signal control remote control receiver, the input connection of electronic governor module and motor module is passed through in the first output that flies to control chip module, fly to control chip module's second output and servo module's input connection, wireless data transmission module and ground control system's I/O both way junction is passed through in the I/O that flies to control chip module, flight control system installs on unmanned helicopter, the utility model discloses it is little to control the degree of difficulty, and the reliability is good with stability.
Description
Technical field
This utility model relates to depopulated helicopter technical field, is specifically related to a kind of depopulated helicopter flight control system.
Background technology
At present, the depopulated helicopter on market all controls by flying hands, due to features such as the structure of helicopter itself and motilities thereof, control so helicopter is extremely difficult, requiring the highest to flying workmanship art, the manipulation difficulty of existing flight control system is big, and reliability and stability is poor.
Summary of the invention
In order to overcome the shortcoming of above-mentioned prior art, the purpose of this utility model is a kind of depopulated helicopter flight control system, and manipulation difficulty is little, and reliability and stability is good.
In order to achieve the above object, the technical scheme that this utility model is taked is:
nullA kind of depopulated helicopter flight control system，Including power module 12，The output of power module 12 and fly to control the first input of chip module 1 and connect，The output flying to control the second input of chip module 1 and GPS module 13 connects，The output flying to control the 3rd input of chip module 1 and pneumatics meter module 8 connects，The output flying to control the 4th input of chip module 1 and magnetic sensor module 7 connects，The output flying to control the 5th input of chip module 1 and inertia measuring module 6 connects，The output flying to control the remote controller 5 that the 6th of chip module 1 enters through remote-control receiver 4 and ground connects，Remote controller 5 controls remote-control receiver 4 by radio wave signal，The first output flying to control chip module 1 is connected by the input of electron speed regulator module 9 and motor module 11，The input flying to control the second output of chip module 1 and steering wheel module 10 connects，The input/output flying to control chip module 1 is bi-directionally connected by the input/output of wireless data transmission module 2 and ground control system 3，Fly to control chip module 1、Wireless data transmission module 2、Remote-control receiver 4、Inertia measuring module 6、Magnetic sensor module 7、Pneumatics meter module 8、Electron speed regulator module 9、Steering wheel module 10、Motor module 11、Power module 12、GPS module 13 connects composition flight control system and is arranged on depopulated helicopter.
The described control chip module 1 that flies uses Atmega1280/2560.
Every flying quality of depopulated helicopter is sent to ground surface end ground control system 3 by described wireless data transmission module 2, monitors the state of flight of depopulated helicopter in real time.
Described remote-control receiver 4 is used for receiving the signal that gps satellite transmits, and depopulated helicopter real-time position information passes to fly to control chip module 1 processes, and obtains the particular location of depopulated helicopter.
Described inertia measuring module 6, magnetic sensor module 7 and pneumatics meter module 8 are with the use of measuring the attitude of depopulated helicopter, course, altitude information, and input flies to control chip module 1.
Described steering wheel module 10 is used for adjusting the attitude of depopulated helicopter.
The beneficial effects of the utility model are: flight control system was employed on many rotor wing unmanned aerial vehicles of symmetrical configuration increasing stability originally, asymmetric due in depopulated helicopter structure, so it has certain difficulty in operability and control, now flight control system is transplanted on depopulated helicopter machine, owing to adding inertia measuring module 6, magnetic sensor module 7 and pneumatics meter module 8 can determine the attitude of unmanned plane in real time, course, altitude information, in GPS module 13 in addition, there is navigation feature, fly to control the data that chip module 1 records according to above-mentioned module, regulate the state of flight of depopulated helicopter in real time, unmanned plane is made automatically to keep homeostasis, whole UAS has higher stability and reliability, so that manipulation difficulty reduces.
Accompanying drawing explanation
Fig. 1 is block diagram of the present utility model.
Detailed description of the invention
Below in conjunction with Figure of description, this utility model is further illustrated.
nullWith reference to Fig. 1，A kind of depopulated helicopter flight control system，Including power module 12，The output of power module 12 and fly to control the first input of chip module 1 and connect，The output flying to control the second input of chip module 1 and GPS module 13 connects，The output flying to control the 3rd input of chip module 1 and pneumatics meter module 8 connects，The output flying to control the 4th input of chip module 1 and magnetic sensor module 7 connects，The output flying to control the 5th input of chip module 1 and inertia measuring module 6 connects，The output flying to control the remote controller 5 that the 6th of chip module 1 enters through remote-control receiver 4 and ground connects，Remote controller 5 controls remote-control receiver 4 by radio wave signal，The first output flying to control chip module 1 is connected by the input of electron speed regulator module 9 and motor module 11，The input flying to control the second output of chip module 1 and steering wheel module 10 connects，The input/output flying to control chip module 1 is bi-directionally connected by the input/output of wireless data transmission module 2 and ground control system 3，Fly to control chip module 1、Wireless data transmission module 2、Remote-control receiver 4、Inertia measuring module 6、Magnetic sensor module 7、Pneumatics meter module 8、Electron speed regulator module 9、Steering wheel module 10、Motor module 11、Power module 12、GPS module 13 connects composition flight control system and is arranged on depopulated helicopter.
The described control chip module 1 that flies uses Atmega1280/2560, and it is exactly Digital Signal Processing computing microprocessor, is the core devices of whole system.
Every flying quality of depopulated helicopter is sent to ground surface end ground control system 3 by described wireless data transmission module 2, monitors the state of flight of depopulated helicopter in real time.
Described remote-control receiver 4 is used for receiving the signal that gps satellite transmits, and depopulated helicopter real-time position information passes to fly to control chip module 1 processes, and obtains the particular location of depopulated helicopter.
Described inertia measuring module 6, magnetic sensor module 7 and pneumatics meter module 8 are with the use of measuring the attitude of depopulated helicopter, course, altitude information, and input flies to control chip module 1.
Described steering wheel module 10 is used for adjusting the attitude of depopulated helicopter.
Described power module 12 is powered to flying control chip module 1.
Operation principle of the present utility model is: in order to increase the operability of depopulated helicopter, now flight control system is implanted on depopulated helicopter, during use, power module 12 is first energized, system initialization is started working, remote-control receiver 4 receives the signal that gps satellite transmits, and real-time position information passed to flies to control chip module 1 process, obtain the particular location of depopulated helicopter, every flying quality of depopulated helicopter is sent to ground surface end ground control system 3 by wireless data transmission module 2, monitors the state of flight of depopulated helicopter in real time.Inertia measuring module 6, magnetic sensor module 7 and pneumatics meter module 8 are with the use of the attitude measuring unmanned plane, course, the data such as height input fly to control chip module 1, fly to control chip module 1 and adjusted the state of depopulated helicopter by computational analysis, it is allowed to safe flight, simultaneously, operator's remote controller 5, remote-control receiver 4 receives radio wave, and be sent to fly to control chip module 1 by corresponding control signal, fly to control chip module 1 to make a response, i.e. control steering wheel module 10 and electron speed regulator module 9 makes corresponding reaction, steering wheel module 10 can adjust aspect direction, electron speed regulator module 9 can control motor module 11, control the power section of depopulated helicopter.
Claims (6)
- null1. a depopulated helicopter flight control system，Including power module (12)，The output of power module (12) and fly to control the first input of chip module (1) and connect，It is characterized in that: the output of the second input and GPS module (13) that fly to control chip module (1) connects，The output flying to control the 3rd input of chip module (1) and pneumatics meter module (8) connects，The output flying to control the 4th input of chip module (1) and magnetic sensor module (7) connects，The output flying to control the 5th input of chip module (1) and inertia measuring module (6) connects，The output flying to control the remote controller (5) that the 6th of chip module (1) enters through remote-control receiver (4) and ground connects，Remote controller (5) controls remote-control receiver (4) by radio wave signal，The first output flying to control chip module (1) is connected by the input of electron speed regulator module (9) and motor module (11)，The input flying to control the second output of chip module (1) and steering wheel module (10) connects，The input/output flying to control chip module (1) is bi-directionally connected by the input/output of wireless data transmission module (2) and ground control system (3)，Fly to control chip module (1)、Wireless data transmission module (2)、Remote-control receiver (4)、Inertia measuring module (6)、Magnetic sensor module (7)、Pneumatics meter module (8)、Electron speed regulator module (9)、Steering wheel module (10)、Motor module (11)、Power module (12)、GPS module (13) connects composition flight control system and is arranged on depopulated helicopter.
- A kind of depopulated helicopter flight control system the most according to claim 1, it is characterised in that fly to control chip module (1) described in: and use Atmega1280/2560.
- A kind of depopulated helicopter flight control system the most according to claim 1, it is characterized in that: every flying quality of depopulated helicopter is sent to ground surface end ground control system (3) by described wireless data transmission module (2), monitor the state of flight of depopulated helicopter in real time.
- A kind of depopulated helicopter flight control system the most according to claim 1, it is characterized in that: described remote-control receiver (4) is used for receiving the signal that gps satellite transmits, and pass to fly to control chip module (1) process by depopulated helicopter real-time position information, obtain the particular location of depopulated helicopter.
- A kind of depopulated helicopter flight control system the most according to claim 1, it is characterized in that: described inertia measuring module (6), magnetic sensor module (7) and pneumatics meter module (8) are with the use of measuring the attitude of depopulated helicopter, course, altitude information, and input flies to control chip module (1).
- A kind of depopulated helicopter flight control system the most according to claim 1, it is characterised in that: described steering wheel module (10) is used for adjusting the attitude of depopulated helicopter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620302568.3U CN205620816U (en) | 2016-04-12 | 2016-04-12 | Unmanned helicopter flight control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620302568.3U CN205620816U (en) | 2016-04-12 | 2016-04-12 | Unmanned helicopter flight control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205620816U true CN205620816U (en) | 2016-10-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620302568.3U Expired - Fee Related CN205620816U (en) | 2016-04-12 | 2016-04-12 | Unmanned helicopter flight control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205620816U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106375026A (en) * | 2016-11-07 | 2017-02-01 | 合肥同想信息技术有限公司 | Digital wireless remote control PWM pulse width modulation terminal |
| CN106996794A (en) * | 2017-04-20 | 2017-08-01 | 佛山科学技术学院 | A kind of depopulated helicopter state monitoring apparatus |
| CN109597422A (en) * | 2018-12-19 | 2019-04-09 | 中国农业大学 | Unmanned tandem helicopter attitude control system and method |
-
2016
- 2016-04-12 CN CN201620302568.3U patent/CN205620816U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106375026A (en) * | 2016-11-07 | 2017-02-01 | 合肥同想信息技术有限公司 | Digital wireless remote control PWM pulse width modulation terminal |
| CN106996794A (en) * | 2017-04-20 | 2017-08-01 | 佛山科学技术学院 | A kind of depopulated helicopter state monitoring apparatus |
| CN109597422A (en) * | 2018-12-19 | 2019-04-09 | 中国农业大学 | Unmanned tandem helicopter attitude control system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161005 Termination date: 20190412 |