CN107092272A - A kind of automated driving system of depopulated helicopter - Google Patents
A kind of automated driving system of depopulated helicopter Download PDFInfo
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- CN107092272A CN107092272A CN201710314655.XA CN201710314655A CN107092272A CN 107092272 A CN107092272 A CN 107092272A CN 201710314655 A CN201710314655 A CN 201710314655A CN 107092272 A CN107092272 A CN 107092272A
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- 230000009286 beneficial effect Effects 0.000 description 2
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- Automation & Control Theory (AREA)
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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Abstract
A kind of automated driving system of depopulated helicopter, the present invention relates to unmanned air vehicle technique field；It also includes airborne controlled module and signal interference module；Described ground control unit also includes Central Control Room control end；Described airborne controlled module is arranged in unmanned plane Central Control Room, and airborne controlled module is connected by wireless signal with Central Control Room control end, while airborne controlled module is connected with unmanned aerial vehicle (UAV) control end；Described signal interference module is connected with Central Control Room control end, meanwhile, signal interference module is connected with terrestrial transmission module；Signal receiving module is provided with described airborne controlled module.Controlled system can be enabled in Emergency time so that unmanned plane can receive the control of aircraft master, it is landed, it is to avoid flight influences taking off for regular flight on aviation track for a long time for it, and its practicality is stronger.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to a kind of automated driving system of depopulated helicopter.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin 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 equipment such as radars, it is tracked, positioned, remote control, remote measurement and Digital Transmission.Can be in radio
Take off or launched with booster rocket as conventional airplane under remote control, can also take aerial deliver to by machine tool and fly.Reclaim
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be reclaimed by remote control parachute or block.Can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..Compared with manned aircraft, it has
Small volume, low cost, it is easy to use, to operational environment require it is low, battlefield survival is stronger the advantages of, enjoy countries in the world army
The favor of team.In several local wars, UAV with its accurate, efficient and nimble scouting, disturb, cheat, search
Rope, school are penetrated and a variety of fight capabilities such as operation under the conditions of informal, play obvious action, and triggered what is emerged in an endless stream
The research of the relevant issues such as art of war, equipment technology.It by with breed in arsenal warship, robot tank, machine personage
One of soldier, computer virus weapon, space-based weapon, laser weapon etc., as on 21 century land battle, sea warfare, air battle, day Haka platform
Key player, more far-reaching influence is caused to following military struggle.
The control loop of current unmanned plane is to be set by professional and technical personnel after program, is navigated according to designed program
OK, when appearance is abnormal in running needs landing, it is necessary to control the professional person of this unmanned plane to be operated, this is to specialty
It is required that it is of a relatively high, when unmanned plane appears in aviation track flying overhead, the normal of aircraft in airport can be influenceed to take off,
Now also need to wait the professional of the unmanned plane to come just operate, this undoubtedly can expend the time, it would be highly desirable to improve.
The content of the invention
It is reasonable in design, make in view of the defects and deficiencies of the prior art, the present invention intends to provide one kind is simple in construction
With the automated driving system of convenient depopulated helicopter, controlled system can be enabled in Emergency time so that unmanned plane can connect
By aircraft, master is controlled, and it is landed, it is to avoid flight influences taking off for regular flight on aviation track for a long time for it, in fact
It is stronger with property.
To achieve the above object, the technical solution adopted by the present invention is：It includes ground control unit and airborne device；Ground
Face control device is connected with airborne device by wireless signal；Described ground control unit is passed comprising owner's control end, ground
Defeated module；Wherein owner's control end is connected with terrestrial transmission module；Described airborne device includes airborne signal receiving module, nothing
Human-machine Control device and unmanned aerial vehicle (UAV) control terminal；Terrestrial transmission module is connected with airborne signal receiving module, and airborne signal receives mould
Block is connected with unmanned aerial vehicle (UAV) control device, and unmanned aerial vehicle (UAV) control device is connected with unmanned aerial vehicle (UAV) control terminal；It also comprising airborne controlled module and
Signal interference module；Described ground control unit also includes Central Control Room control end；Described airborne controlled module is arranged on nothing
In man-machine Central Control Room, and airborne controlled module is connected by wireless signal with Central Control Room control end, at the same airborne controlled module with
Unmanned aerial vehicle (UAV) control end is connected；Described signal interference module is connected with Central Control Room control end, meanwhile, signal interference module and ground
Transport module is connected；Signal receiving module is provided with described airborne controlled module.
Further, described unmanned aerial vehicle (UAV) control terminal includes unmanned plane during flying navigation system, unmanned plane speed control system
System, unmanned plane jacking system, unmanned plane system, unmanned plane safety monitoring system, unmanned plane alarm system；Wherein institute
The unmanned plane jacking system stated is connected with unmanned plane controlled module.
Further, described unmanned plane controlled module is connected with unmanned plane alarm system.
Further, the signal frequency range in described terrestrial transmission module is different from signal reception mould in airborne controlled module
The manipulated signal frequency range that block is received.
After said structure, the present invention has the beneficial effect that：A kind of automatic Pilot of depopulated helicopter of the present invention
System, can enable controlled system in Emergency time so that unmanned plane can receive the control of aircraft master, it is landed,
Avoid taking off for its long-term flight influence regular flight on aviation track, its practicality is stronger, the present invention have it is simple in construction,
It is reasonable to set, the advantages of low manufacture cost.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, without having to pay creative labor, may be used also
To obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is the structured flowchart of the present invention.
Fig. 2 is the CONSTRUCTED SPECIFICATION block diagram of the present invention.
Fig. 3 is unmanned aerial vehicle (UAV) control terminal and the connection diagram of unmanned plane controlled module in the present invention.
Description of reference numerals：
Ground control unit 1, airborne device 2, owner's control end 4, terrestrial transmission module 5, airborne letter
Number receiving module 6, unmanned aerial vehicle (UAV) control device 7, unmanned aerial vehicle (UAV) control terminal 8, Central Control Room control end 9,
Signal interference module 10, signal receiving module 11, unmanned plane during flying navigation system 12, unmanned plane speed
Control system 13, unmanned plane jacking system 14, unmanned plane system 15, unmanned plane is spent to supervise safely
Examining system 16, unmanned plane alarm system 17.
Embodiment
The present invention is further illustrated below in conjunction with the accompanying drawings.
Referring to as shown in Figure 1-Figure 3, the technical scheme that present embodiment is used is：It includes ground control unit 1
With airborne device 2；Ground control unit 1 is connected with airborne device 2 by wireless signal；Described ground control unit 1 is included
Owner's control end 4, terrestrial transmission module 5；Wherein owner's control end 4 is connected with terrestrial transmission module 5；Described airborne device 2
Include airborne signal receiving module 6, unmanned aerial vehicle (UAV) control device 7 and unmanned aerial vehicle (UAV) control terminal 8；Terrestrial transmission module 5 and airborne signal
Receiving module 6 is connected, and airborne signal receiving module 6 is connected with unmanned aerial vehicle (UAV) control device 7, unmanned aerial vehicle (UAV) control device 7 and unmanned aerial vehicle (UAV) control
Terminal 8 is connected；It also includes airborne controlled module 3 and signal interference module 10；Described ground control unit 1 also includes middle control
Room control end 9；Described airborne controlled module 3 is arranged in unmanned plane Central Control Room, and airborne controlled module 3 passes through wireless signal
It is connected with Central Control Room control end 9, while airborne controlled module 3 is connected with unmanned aerial vehicle (UAV) control end；Described signal interference module 10
It is connected with Central Control Room control end 9, meanwhile, signal interference module 10 is connected with terrestrial transmission module 5；Described airborne controlled module
Signal receiving module 11 is provided with 3.
Further, described unmanned aerial vehicle (UAV) control terminal 8 includes unmanned plane during flying navigation system 12, unmanned plane speed control
System 13, unmanned plane jacking system 14, unmanned plane system 15, unmanned plane safety monitoring system 16, unmanned plane danger warning
System 17；Wherein described unmanned plane jacking system 14 is connected with unmanned plane controlled module 3.
Further, described unmanned plane controlled module 3 is connected with unmanned plane alarm system 17.
Further, the signal frequency range in described terrestrial transmission module 5 is different from signal reception in airborne controlled module 3
The manipulated signal frequency range that module 11 is received.
The operation principle of present embodiment：Be required for controlling wherein when every frame unmanned plane is produced indoor location nobody
Machine controlled module 3, when unmanned plane stays flight for a long time on flight track, airport employe can pass through Central Control Room control
End 9 processed can disturb the signal frequency that ground transport module 5 is sent by signal interference module 10, so that cutting machine main control end
The control of 4 pairs of unmanned planes, is simultaneously emitted by being different from the signal for the different frequency range that owner's control end 4 is sent to airborne controlled module 3,
Unmanned plane jacking system 14 in the airborne control unmanned aerial vehicle (UAV) control of controlled module 3 end 8, so as to control unmanned plane to land, while can
To control unmanned plane alarm system 17, start hazard detection system, so that owner's control end 4 is notified, when unmanned plane is strong
After system landing, the aircraft on airport then can normally take off, and after airport aircraft all normal end of runs, airport employe is also
By Central Control Room control end 9 unmanned plane can be controlled to take off, last shutdown signal interference module 10, unmanned plane then departs from Central Control Room
Control, in the control range for being again introduced into owner's control end 4.
After said structure, present embodiment has the beneficial effect that：Described in present embodiment it is a kind of nobody
The automated driving system of helicopter, can enable controlled system in Emergency time so that unmanned plane can receive aircraft master
Control, it is landed, it is to avoid flight influence regular flight is taken off on aviation track for a long time for it, and its practicality is stronger, this
Invention has simple in construction, and it is reasonable to set, the advantages of low manufacture cost.
It is described above, it is merely illustrative of the technical solution of the present invention and unrestricted, those of ordinary skill in the art are to this hair
Other modifications or equivalent substitution that bright technical scheme is made, without departing from the spirit and scope of technical solution of the present invention,
It all should cover among scope of the presently claimed invention.
Claims (4)
1. a kind of automated driving system of depopulated helicopter, it includes ground control unit and airborne device；Ground control unit
It is connected with airborne device by wireless signal；Described ground control unit includes owner's control end, terrestrial transmission module；Wherein
Owner's control end is connected with terrestrial transmission module；Described airborne device includes airborne signal receiving module, unmanned aerial vehicle (UAV) control device
With unmanned aerial vehicle (UAV) control terminal；Terrestrial transmission module is connected with airborne signal receiving module, airborne signal receiving module and unmanned plane
Controller is connected, and unmanned aerial vehicle (UAV) control device is connected with unmanned aerial vehicle (UAV) control terminal；It is characterized in that：It also comprising airborne controlled module and
Signal interference module；Described ground control unit also includes Central Control Room control end；Described airborne controlled module is arranged on nothing
In man-machine Central Control Room, and airborne controlled module is connected by wireless signal with Central Control Room control end, at the same airborne controlled module with
Unmanned aerial vehicle (UAV) control end is connected；Described signal interference module is connected with Central Control Room control end, meanwhile, signal interference module and ground
Transport module is connected；Signal receiving module is provided with described airborne controlled module.
2. a kind of automated driving system of depopulated helicopter according to claim 1, it is characterised in that：Described unmanned plane
Control terminal includes unmanned plane during flying navigation system, unmanned plane speed control system, unmanned plane jacking system, unmanned plane system
System, unmanned plane safety monitoring system, unmanned plane alarm system；Wherein described unmanned plane jacking system is controlled with unmanned plane
Module is connected.
3. a kind of automated driving system of depopulated helicopter according to claim 2, it is characterised in that：Described unmanned plane
Controlled module is connected with unmanned plane alarm system.
4. a kind of automated driving system of depopulated helicopter according to claim 1, it is characterised in that：Described ground is passed
Signal frequency range in defeated module is different from the manipulated signal frequency range that signal receiving module is received in airborne controlled module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710314655.XA CN107092272B (en) | 2017-05-06 | 2017-05-06 | Automatic piloting system of unmanned helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710314655.XA CN107092272B (en) | 2017-05-06 | 2017-05-06 | Automatic piloting system of unmanned helicopter |
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| Publication Number | Publication Date |
|---|---|
| CN107092272A true CN107092272A (en) | 2017-08-25 |
| CN107092272B CN107092272B (en) | 2021-03-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710314655.XA Active CN107092272B (en) | 2017-05-06 | 2017-05-06 | Automatic piloting system of unmanned helicopter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109429036A (en) * | 2017-09-01 | 2019-03-05 | 齐心 | A kind of counter system of video monitoring transmission |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100489736B1 (en) * | 2002-11-20 | 2005-05-16 | 한국항공우주연구원 | Flight termination System of the Unmanned Airship |
| CN104808682A (en) * | 2015-03-10 | 2015-07-29 | 成都市优艾维机器人科技有限公司 | Small rotor unmanned aerial vehicle autonomous obstacle avoidance flight control system and control method |
| CN205049892U (en) * | 2015-10-19 | 2016-02-24 | 赵文洁 | Unmanned aerial vehicle emergency control system |
| CN205751276U (en) * | 2016-05-16 | 2016-11-30 | 北华大学 | A kind of movable unmanned helicopter flight range limits system |
| CN106228809A (en) * | 2016-08-11 | 2016-12-14 | 安徽钰龙信息科技有限公司 | A kind of novel on-vehicle unmanned plane overload control transfinites workstation system |
| CN205945766U (en) * | 2016-08-23 | 2017-02-08 | 深圳市东楠科技发展有限公司 | Unmanned aerial vehicle's taboo flies defense system |
-
2017
- 2017-05-06 CN CN201710314655.XA patent/CN107092272B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100489736B1 (en) * | 2002-11-20 | 2005-05-16 | 한국항공우주연구원 | Flight termination System of the Unmanned Airship |
| CN104808682A (en) * | 2015-03-10 | 2015-07-29 | 成都市优艾维机器人科技有限公司 | Small rotor unmanned aerial vehicle autonomous obstacle avoidance flight control system and control method |
| CN205049892U (en) * | 2015-10-19 | 2016-02-24 | 赵文洁 | Unmanned aerial vehicle emergency control system |
| CN205751276U (en) * | 2016-05-16 | 2016-11-30 | 北华大学 | A kind of movable unmanned helicopter flight range limits system |
| CN106228809A (en) * | 2016-08-11 | 2016-12-14 | 安徽钰龙信息科技有限公司 | A kind of novel on-vehicle unmanned plane overload control transfinites workstation system |
| CN205945766U (en) * | 2016-08-23 | 2017-02-08 | 深圳市东楠科技发展有限公司 | Unmanned aerial vehicle's taboo flies defense system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109429036A (en) * | 2017-09-01 | 2019-03-05 | 齐心 | A kind of counter system of video monitoring transmission |
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| CN107092272B (en) | 2021-03-26 |
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