CN206741234U - A kind of manned vehicle automatic safety control system - Google Patents
A kind of manned vehicle automatic safety control system Download PDFInfo
- Publication number
- CN206741234U CN206741234U CN201720255351.6U CN201720255351U CN206741234U CN 206741234 U CN206741234 U CN 206741234U CN 201720255351 U CN201720255351 U CN 201720255351U CN 206741234 U CN206741234 U CN 206741234U
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- China
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- control system
- humidity
- central control
- manned vehicle
- flight
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Abstract
The utility model discloses a kind of manned vehicle automatic safety control system and its control method,Including central control system,The pitot meter of the central control system and measurement air speed value,The temperature of measurement temperature humidity,Humidity sensor,The GPS of measurement position information is connected,The central control system output end is connected with electric machine controller,The electric machine controller output end is connected with motor,The utility model take off before to wind speed and ambient humidity inspection,In the case of takeoff condition is not met,Lock main motor throttle,Forbid taking off,Environment is checked in flight course,When aircraft can not automatically adjust balance or excessive humidity,Operator is reminded by sound and screen,And reduce speed traveling,Prompt operator that nearby reduction of speed lands,The utility model can be to environment and the flight environment of vehicle progress accurate feedback of taking off,The personal safety of operator is ensured.
Description
Technical field
The utility model belongs to the safety protection field of aircraft, and in particular to a kind of manned vehicle automatic safe control
System and its control method.
Background technology
General Aviation industry is in the ascendant both at home and abroad at present, and developed country have developed sole flight with their own characteristics in succession
Device, familiar Martin's flight knapsack such as everybody, German develop more rotor manned aircraft, Japanese develop one
Aircraft, and the individual lift device that China develops.
But above-mentioned aircraft all only considers flight, the not no condition to flight and in particular circumstances, flight control system
How system should control, and could ensure the safety of people to greatest extent.
Manned vehicle in the market all forbids function of taking off automatically without design, i.e., wind speed measurement is more than a fixed number
Value（Strong wind weather）Aircraft is forbidden taking off automatically afterwards；Air humidity exceedes certain numerical value（Thunderstorm weather）Forbid taking off；And
The automatic safe protective measure for pre- strong wind and thunderstorm weather control system of in-flight dashing forward, the safety of people is ensured to greatest extent.
The content of the invention
The utility model proposes that the purpose is to provide a kind of manned vehicle certainly to solve the problems, such as that prior art is present
Dynamic safety control system and its control method.
The technical solution of the utility model is：A kind of manned vehicle automatic safety control system, including center control system
System, the central control system and the measurement pitot meter of air speed value, the temperature and relative humidity of measurement temperature humidity, measurement position
The GPS of information is connected, and the central control system output end is connected with electric machine controller, the electric machine controller output end and electricity
Machine is connected.
The feeder ear of the central control system is connected with power supply.
The central control system is connected with display screen, and central control system is by air speed value, temperature humidity value, positional information
Export to display screen.
The utility model take off before to wind speed and ambient humidity inspection, in the case of takeoff condition is not met, lock main electricity
Machine oil door, forbid taking off, environment is checked in flight course, aircraft can not automatically adjust balance or humidity is excessive
When, operator is reminded by sound and screen, and speed traveling is reduced, prompt operator that nearby reduction of speed lands, this practicality is new
Type can ensure the personal safety of operator to environment and the flight environment of vehicle progress accurate feedback of taking off.
Brief description of the drawings
Fig. 1 is the connection diagram of control system in the utility model；
Fig. 2 is pre-flight method flow diagram in control method in the utility model；
Fig. 3 is the method flow diagram in control method in-flight in the utility model；
Wherein：
The electric machine controller of 1 central control system 2
The temperature and relative humidity of 3 motor 4
The GPS of 5 pitot meter 6
The power supply of 7 display screen 8.
Embodiment
Hereinafter, the utility model is described in detail with embodiment referring to the drawings：
As shown in figure 1, a kind of manned vehicle automatic safety control system, including central control system 1, the center control
System 1 processed and the measurement pitot meter 5 of air speed value, the temperature and relative humidity 4 of measurement temperature humidity, the GPS6 of measurement position information
It is connected, the output end of central control system 1 is connected with electric machine controller 2, the output end of electric machine controller 2 and the phase of motor 3
Even.
The feeder ear of the central control system 1 is connected with power supply 8.
The central control system 1 is connected with display screen 7, and central control system 1 is by air speed value, temperature humidity value, position
Information is exported to display screen 7.
As shown in Figure 2,3, the control method of above-mentioned a kind of manned vehicle automatic safety control system, including following step
Suddenly：
Before manned vehicle takes off, air speed value, humidity value are acquired successively, and judge whether to meet takeoff condition；
In manned vehicle flight course, air speed value, humidity value are acquired and whether real-time judge possesses flight bar
Part.
Before the manned vehicle takes off, air speed value, humidity value are acquired successively, and judge whether to meet the bar that takes off
Part comprises the following steps：
（ⅰ）Program initialization
Initialize and set safe take-off wind speed 10m/s, setting safe take-off humidity 80%；
（ⅱ）Pitot meter obtains wind speed information
Pitot meter 5 measures to playing enclave air speed value；
（ⅲ）Pitot meter sends the air speed value of acquisition to central control system；
（ⅳ）Central control system is analyzed air speed data；
（ⅴ）Whether safe take-off wind speed 10m/s is less than；
Step（ⅱ）In wind speed information be less than safe take-off wind speed 10m/s, continue executing with step（ⅵ）；Step（ⅱ）In
Wind speed information be more than safe take-off wind speed 10m/s, perform step（ⅹⅰ）；
（ⅵ）Epidemic disaster meter obtains humidity information
Temperature and relative humidity 4 measures to playing enclave humidity；
（ⅶ）Epidemic disaster meter sends the humidity value of acquisition to central processing system；
（ⅷ）Central control system is analyzed humidity data；
（ⅸ）Whether safe take-off humidity 80% is less than；
Step（ⅵ）The humidity information of middle acquisition is less than safe take-off humidity 80%, continues executing with step（ⅹ）；Step（ⅵ）
The humidity information of middle acquisition is more than safe take-off humidity 80%, continues executing with step（ⅹⅰ）；
（ⅹ）Carry out preceding preparation of flying
（ⅹⅰ）Throttle is locked, forbids taking off.
In the manned vehicle flight course, air speed value, humidity value are acquired and real-time judge whether possess it is winged
Row condition, comprises the following steps：
（ⅰ）Program initialization
Safe flight wind speed information is initialized, safe flight wind speed information is rated wind velocity 10m/s and the duration is formed
Beam wind condition is less than 0.2s；Initialize safe flight humidity information, safe flight humidity information be humidity definite value 80% and continue when
Between form condition of raining 1s；
（ⅱ）Pitot meter obtains wind speed information；
（ⅲ）Pitot meter sends the air speed value of acquisition to central control system；
（ⅳ）Central control system is analyzed air speed data；
（ⅴ）Whether safe flight wind speed information is less than
Step（ⅱ）In wind speed information be less than safe flight wind speed information, i.e., rated wind velocity less than 10m/s and it is lasting when
Between form beam wind condition be less than 0.2s, continue executing with step（ⅵ）；Step（ⅱ）In wind speed information be more than safe flight wind speed
Information, i.e. rated wind velocity form beam wind condition and are more than 0.2s higher than 10m/s and duration, and aircraft enters from steady pattern, after
It is continuous to perform step（ⅹⅰ）；
（ⅵ）Hygrothermograph obtains humidity information；
（ⅶ）Hygrothermograph gives the humidity value bed of acquisition to central control system；
（ⅷ）Central control system is analyzed humidity data；
（ⅸ）Whether safe flight humidity information is less than
Step（ⅵ）In humidity information be less than safe flight humidity information, i.e. humidity definite value is less than 80% and duration
Form condition of raining and be less than 1s, continue executing with step（ⅹ）；Step（ⅵ）In humidity information be more than safe flight humidity information,
I.e. humidity definite value is higher than 80% and the duration forms condition of raining and is more than 1s, continues executing with step（ⅹⅱ）；
（ⅹ）Perform flight；
（ⅹⅰ）Whether central control system inspection can maintain to balance from steady pattern
It can maintain to balance from steady pattern, continue executing with step（ⅵ）；It can not maintain to balance from steady pattern, perform step
（ⅹⅱ）；
（ⅹⅱ）Speed traveling prompting operator is reduced nearby to land.
The central control system 1 is also connected with prefabricated audible alarm module.
The utility model take off before to wind speed and ambient humidity inspection, in the case of takeoff condition is not met, lock main electricity
Machine oil door, forbid taking off, environment is checked in flight course, aircraft can not automatically adjust balance or humidity is excessive
When, operator is reminded by sound and screen, and speed traveling is reduced, prompt operator that nearby reduction of speed lands, this practicality is new
Type can ensure the personal safety of operator to environment and the flight environment of vehicle progress accurate feedback of taking off.
Claims (3)
1. a kind of manned vehicle automatic safety control system, including central control system（1）, it is characterised in that：The center
Control system（1）Pitot meter with measuring air speed value（5）, measurement temperature humidity temperature and relative humidity（4）, measurement position letter
The GPS of breath（6）It is connected, the central control system（1）Output end and electric machine controller（2）It is connected, the electric machine controller（2）
Output end and motor（3）It is connected.
A kind of 2. manned vehicle automatic safety control system according to claim 1, it is characterised in that：The center control
System processed（1）Feeder ear and power supply（8）It is connected.
A kind of 3. manned vehicle automatic safety control system according to claim 1, it is characterised in that：The center control
System processed（1）With display screen（7）It is connected, central control system（1）Air speed value, temperature humidity value, positional information are exported to aobvious
Display screen（7）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720255351.6U CN206741234U (en) | 2017-03-16 | 2017-03-16 | A kind of manned vehicle automatic safety control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720255351.6U CN206741234U (en) | 2017-03-16 | 2017-03-16 | A kind of manned vehicle automatic safety control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206741234U true CN206741234U (en) | 2017-12-12 |
Family
ID=60557656
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720255351.6U Expired - Fee Related CN206741234U (en) | 2017-03-16 | 2017-03-16 | A kind of manned vehicle automatic safety control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206741234U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112068601A (en) * | 2020-10-20 | 2020-12-11 | 北京卫通新科测控技术有限公司 | Navigation control system for fixed-wing unmanned aerial vehicle |
-
2017
- 2017-03-16 CN CN201720255351.6U patent/CN206741234U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112068601A (en) * | 2020-10-20 | 2020-12-11 | 北京卫通新科测控技术有限公司 | Navigation control system for fixed-wing unmanned aerial vehicle |
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Legal Events
| 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: 20171212 Termination date: 20200316 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |