CN209356901U - A kind of three rotor wing unmanned aerial vehicle control systems - Google Patents
A kind of three rotor wing unmanned aerial vehicle control systems Download PDFInfo
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- CN209356901U CN209356901U CN201920435805.7U CN201920435805U CN209356901U CN 209356901 U CN209356901 U CN 209356901U CN 201920435805 U CN201920435805 U CN 201920435805U CN 209356901 U CN209356901 U CN 209356901U
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Abstract
A kind of three rotor wing unmanned aerial vehicle control systems, including executing terminal and operating terminal, the execution terminal includes the first main control module, first main control module is connected with electron speed regulator, first communication module, obstacle sensor, pressure-altitude sensor, flash lamp, GPS module, electric power detection module and the first power module, the electron speed regulator is connected with power device, the electric power detection module is also connect with the first power module, the operating terminal includes the second main control module, second main control module is connected with input module, second communication module, indicator lamp groups and second power supply module, the utility model has barrier, height detection function simultaneously can be carried out real-time prompting, and it is easy to control, cruising ability is strong.
Description
Technical field
The utility model belongs to unmanned aerial vehicle (UAV) control technical field, and in particular to a kind of three rotor wing unmanned aerial vehicle control systems.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, it is tracked, is positioned, is remotely controlled, telemetering and Digital Transmission, unmanned plane it is usual
The local operation, such as Fight Fire in Forest, structural fire fighting etc. for needing to have barrier and high-altitude, if do not take corresponding failure and
Height detection means, unmanned plane often face collision and the possibility beyond control height during operation.
Utility model content
A kind of three rotor wing unmanned aerial vehicle control systems are provided the purpose of the utility model is to overcome the deficiencies in the prior art, this
Utility model has the function of barrier, height detection and can be carried out real-time prompting, and easy to control, and cruising ability is strong.
The technical solution of the utility model is as follows: a kind of three rotor wing unmanned aerial vehicle control systems, including executes terminal and operation
Terminal, the execution terminal include the first main control module, and first main control module is connected with electron speed regulator, the first communication mould
Block, obstacle sensor, pressure-altitude sensor, flash lamp, GPS module, electric power detection module and the first power module, the electricity
Sub- governor is connected with power device, and the electric power detection module is also connect with the first power module, and the operating terminal includes
Second main control module, second main control module are connected with input module, second communication module, indicator lamp groups and second source mould
Block.
Preferably, the power device includes motor and the screw wing that is mounted on motor, the motor and electronic speed regulation
Device connection.
Preferably, second main control module is also connected with alarm.
Preferably, the indicator lamp groups include obstruction lights, height indicator light and low battery indicator light.
Preferably, first power module and second power supply module are all made of charged lithium cells group.
The utility model has the beneficial effects that
(1) by the utility model install obstacle sensor and pressure-altitude sensor, can to barrier and height into
Row real-time detection, and real-time prompting can be carried out to operator by flash lamp, indicator lamp groups and the alarm of setting, guarantee this
Utility model using safe；
(2) operating terminal is realized by first communication module and second communication module and executes the wireless connection of terminal, control
System is convenient, easy to operate.
In short, the utility model has the function of barrier, height detection and can be carried out real-time prompting, and easy to control, continue
Boat ability is strong.
Detailed description of the invention
Fig. 1 is the execution terminal control block diagram of the utility model；
Fig. 2 is the operating terminal control block diagram of the utility model；
Fig. 3 is the composition block diagram of the utility model indicator lamp groups.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
As shown in Figure 1-3, a kind of three rotor wing unmanned aerial vehicle control systems, including execute terminal and operating terminal, the execution
Terminal includes the first main control module, and first main control module is connected with electron speed regulator, first communication module, obstacle sensing
Device, pressure-altitude sensor, flash lamp, GPS module, electric power detection module and the first power module, the electron speed regulator connect
It is connected to power device, the electric power detection module is also connect with the first power module, and the operating terminal includes the second master control mould
Block, second main control module are connected with input module, second communication module, indicator lamp groups and second power supply module.
In the present embodiment,
The execution terminal is set on three rotor wing unmanned aerial vehicles, execute terminal and operating terminal by first communication module and
Second communication module carries out the wireless transmission of data, signal, execute the first main control module being arranged in terminal and operating terminal and
Second main control module is all made of MSP430F169IPM chip；
The obstacle sensor and pressure-altitude sensor be respectively used at a distance from detection unmanned plane and peripheral obstacle with
And the height between ground, the GPS module are used for the positioning of unmanned plane, the electric power detection module is used for the first power supply mould
The detection of block electricity, the flash lamp be used for when night unmanned plane is closer from barrier, with a distance from ground farther out when and battery
The sparkling prompting under either case when electricity is lower；
The input module is used for the input instructed to unmanned plane during flying, and the indicator lamp groups are used for the improper shape of unmanned plane
Instruction under state, specifically include obstruction lights, height indicator light and low battery indicator light, i.e., when unmanned plane from barrier compared with
When close, apart from ground farther out when and battery capacity it is lower when correspond to indicator light and light, to prompt operator；
The power device includes motor and the screw wing that is mounted on motor, and the motor is connect with electron speed regulator,
First main control module controls the revolving speed of motor and screw wing by electron speed regulator；
Second main control module is also connected with alarm, and when any indicator light lights, alarm will issue alarm
Signal prevents operator from cannot find the case where indicator light lights at the first time；
First power module and second power supply module are all made of charged lithium cells group, can fully ensure that execute terminal and
The electric power of operating terminal is continued a journey.
When the utility model is implemented:
Flight directive is issued to unmanned plane by the input module (key or control stick) of operating terminal, command signal passes through
Second communication module issues, and the first main control module is received and be transmitted to through the first transmission module, the first main control module passes through electronics
Governor controls the rotation of motor and screw wing to complete the flight of unmanned plane, when unmanned plane is in flight course, obstacle
Sensor, pressure-altitude sensor and electric power detection module can be measured in real time unmanned plane situation, the data information of detection
It can be transmitted to the first main control module, the first main control module analyzes and determines data, when judging result is unmanned plane from obstacle
When object is closer, apart from ground farther out when and battery capacity it is lower when, then flash lamp can constantly flash remind operator, simultaneously
The data of detection can also be issued through first communication module, receive and be transmitted to the second main control module through second communication module, and second
Main control module can be controlled corresponding obstruction lights, height indicator light and low battery indicator light and lighted by judgement, when times
When one indicator light lights, alarm can issue alarm signal for reminding operator to carry out cut-through object or behaviour of making a return voyage simultaneously
Make.
Although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should all
It is included within the scope of protection of this utility model.
Claims (5)
1. a kind of three rotor wing unmanned aerial vehicle control systems, it is characterised in that: including executing terminal and operating terminal, the execution terminal
Including the first main control module, first main control module is connected with electron speed regulator, first communication module, obstacle sensor, gas
Pressure height sensor, flash lamp, GPS module, electric power detection module and the first power module, the electron speed regulator are connected with dynamic
Power device, the electric power detection module are also connect with the first power module, and the operating terminal includes the second main control module, described
Second main control module is connected with input module, second communication module, indicator lamp groups and second power supply module.
2. three rotor wing unmanned aerial vehicles control system according to claim 1, it is characterised in that: the power device includes motor
With the screw wing being mounted on motor, the motor is connect with electron speed regulator.
3. three rotor wing unmanned aerial vehicles control system according to claim 1, it is characterised in that: second main control module also connects
It is connected to alarm.
4. three rotor wing unmanned aerial vehicles control system according to claim 1, it is characterised in that: the indicator lamp groups include obstacle
Indicator light, height indicator light and low battery indicator light.
5. three rotor wing unmanned aerial vehicles control system according to claim 1, it is characterised in that: first power module and
Two power modules are all made of charged lithium cells group.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920435805.7U CN209356901U (en) | 2019-04-02 | 2019-04-02 | A kind of three rotor wing unmanned aerial vehicle control systems |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920435805.7U CN209356901U (en) | 2019-04-02 | 2019-04-02 | A kind of three rotor wing unmanned aerial vehicle control systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209356901U true CN209356901U (en) | 2019-09-06 |
Family
ID=67804621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920435805.7U Expired - Fee Related CN209356901U (en) | 2019-04-02 | 2019-04-02 | A kind of three rotor wing unmanned aerial vehicle control systems |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209356901U (en) |
-
2019
- 2019-04-02 CN CN201920435805.7U patent/CN209356901U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190906 |
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| CF01 | Termination of patent right due to non-payment of annual fee |