CN106094870A - A kind of flight control system based on wireless telecommunications unmanned plane - Google Patents
A kind of flight control system based on wireless telecommunications unmanned plane Download PDFInfo
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- CN106094870A CN106094870A CN201610705756.5A CN201610705756A CN106094870A CN 106094870 A CN106094870 A CN 106094870A CN 201610705756 A CN201610705756 A CN 201610705756A CN 106094870 A CN106094870 A CN 106094870A
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- unmanned plane
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- control centre
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 14
- 241001465754 Metazoa Species 0.000 claims abstract description 11
- 230000000875 corresponding effect Effects 0.000 claims abstract description 4
- 230000004888 barrier function Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 241000700605 Viruses Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Classifications
-
- 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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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
The invention discloses a kind of flight control system based on wireless telecommunications unmanned plane, including control centre and implementation center, it is characterized in that: implementation center includes receiver module, A/D module, trigger, triggering sound wave device, performs module, and wherein said receiver module receives the instruction of control centre and is sent to perform module；In the region of described A/D module collection circumference centered by unmanned plane 85 105 miles, all animal informations are transferred to the computer of control centre；Any foreign object of described trigger enters in the region of the circumference 5 miles centered by unmanned plane, flip-flop toggle, is simultaneously emitted by instruction to triggering sound wave device and the computer of control centre；Described triggering sound wave device receives the instruction of trigger and sends infrasonic wave；Described execution module receives the instruction of implementation center's receiver module and makes corresponding actions.The main information of A/D module be the circumference 85 105 miles centered by unmanned plane region in all animal informations.
Description
Technical field
The present invention relates to the flight control system of a kind of unmanned plane, be specifically related to a kind of based on wireless telecommunications unmanned plane fly
Row control system.
Background technology
UAV is a kind of based on wireless remotecontrol or by the most manned aircraft of self programme-control.Grinding of it
Make merit and battlefield uses, open " the untouchable war taken as the leading factor with remote attack smart weapon, intelligent weapon
Strive " new page.Compared with manned aircraft, it has, and volume is little, cost is low, easy to use, low to operational environment requirement, battlefield
The advantages such as survival ability is stronger, enjoy the favor of all armies in the world.In several local wars, UAV is accurate with it
Really, efficient and nimble scouting, disturb, cheat, search for, school is penetrated and the multiple fight capability such as operation under the conditions of informal, send out
Wave obvious action, and cause the research of the relevant issues such as the art of war, the equipment technology that emerge in an endless stream.It will with breed
In arsenal warship, robot tank, robot soldier, computer virus weapon, space-based weapon, laser weapon etc. together, become
For the key player on 21 century land battle, sea warfare, air battle, sky Haka platform, following military struggle is caused the most far-reaching shadow
Ring.UAV is called for short " unmanned plane ", is to utilize infrared ray electric remote control equipment and the presetting apparatus provided for oneself to handle
The most manned aircraft.Current most of civilian unmanned aerial vehicle (UAV) control is straight by infrared line data radio station between earth station and unmanned plane
Tap into row data communication, then pass through earth station's software editing flight plan and upload to UAV Flight Control device.Unmanned plane makes
With more and more extensive, but the aerial animal attack condition more than two to unmanned plane.
All air securities to unmanned plane are flown and are avoided animal attacks problem to become the problem that a gate value must be studied.
Summary of the invention
The technical problem to be solved is that animal attacks is avoided in air security flight, it is therefore intended that provide a kind of base
In the flight control system of wireless telecommunications unmanned plane, solve the problem that animal attacks is avoided in air security flight.
The present invention is achieved through the following technical solutions:
A kind of flight control system based on wireless telecommunications unmanned plane, including control centre and implementation center, it is characterised in that: hold
Row center includes receiver module, A/D module, trigger, triggering sound wave device, performs module, and wherein said receiver module receives and controls
The instruction at center is sent to perform module；In the region of described A/D module collection circumference 85-105 mile centered by unmanned plane
All animal informations are transferred to the computer of control centre；Any foreign object of described trigger enters the circumference centered by unmanned plane
In the region of 5 miles, flip-flop toggle, it is simultaneously emitted by instruction to triggering sound wave device and the computer of control centre；Described triggering
Sound wave device receives the instruction of trigger and sends infrasonic wave；Described execution module receives the instruction of implementation center's receiver module and does
Go out corresponding actions.The main information of A/D module be the circumference 85-105 mile centered by unmanned plane region in all animals letter
Breath.In addition, it can include some other additional informations, such as course, air speed, wind speed, wind direction and aircraft ambient temperature etc..Trigger
Device processes the foreign object in the region of the circumference 5 miles centered by unmanned plane and to send instruction main to computer with trigger sound wave device, sends out
Go out infrasonic wave to attack to force back and hit exotic, and after computer receives this information, automatically do the course line made new advances adjust and keep away as far as possible
Exempt from.
Described execution module arranges automatic collision function, and when unmanned plane is less than 1M with obstacle distance, unmanned plane suspends
All instructions are also return 5 meters from trend barrier and are further continued for receiving other instructions.Carry the life-span of collision prevention function protection unmanned plane,
Work on after returning 5M and improve safety coefficient.
Described command encoder and decoder all use STC89C51 single-chip microcomputer, have the CPU of 18 in 51 single-chip microcomputers, can
To carry out the process of variable, it is also 4KBROM with program storage.
The present invention compared with prior art, has such advantages as and beneficial effect:
1, a kind of flight control system based on wireless telecommunications unmanned plane of the present invention, carries the longevity of collision prevention function protection unmanned plane
Life, works on after returning 5M and improves safety coefficient；
2, a kind of flight control system based on wireless telecommunications unmanned plane of the present invention, arranges triggering sound wave device and sends infrasonic wave and attack and force
Move back and hit exotic, and after computer receives this information, automatically do the course line that makes new advances adjust and avoid as far as possible；
3, a kind of flight control system based on wireless telecommunications unmanned plane of the present invention, uses in 51 single-chip microcomputer STC89C51 and has 18
The CPU of position, can carry out the process of variable, is also 4KBROM with program storage.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with embodiment, the present invention is made
Further describing in detail, the exemplary embodiment of the present invention and explanation thereof are only used for explaining the present invention, are not intended as this
The restriction of invention.
Embodiment
A kind of flight control system based on wireless telecommunications unmanned plane of the present invention, including control centre and implementation center, holds
Row center includes that receiver module uses STC89C51, A/D module to use TDF-895L, trigger to use LLI201-D, trigger sound wave
Device uses YB-589, performs module employing computer, and wherein said receiver module receives the instruction of control centre and is sent to perform
Module；In the region of described A/D module collection circumference 85-105 mile centered by unmanned plane, all animal informations are transferred to control
The computer at center processed；Any foreign object of described trigger enters in the region of the circumference 5 miles centered by unmanned plane, trigger
Start, be simultaneously emitted by instruction to triggering sound wave device and the computer of control centre；Described triggering sound wave device receives the finger of trigger
Make and send infrasonic wave；Described execution module receives the instruction of implementation center's receiver module and makes corresponding actions.A/D module
Main information be the circumference 85-105 mile centered by unmanned plane region in all animal informations.In addition, it can include one
A little other additional informations, such as course, air speed, wind speed, wind direction and aircraft ambient temperature etc..Centered by trigger processes unmanned plane
Have an area of the foreign object in the region of 5 miles and to send instruction main to computer with trigger sound wave device, send infrasonic wave attack force back hit external
Thing, and after computer receives this information, automatically do the course line that makes new advances adjust and avoid as far as possible.
Above-described detailed description of the invention, has been carried out the purpose of the present invention, technical scheme and beneficial effect further
Describe in detail, be it should be understood that the detailed description of the invention that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, all should comprise
Within protection scope of the present invention.
Claims (3)
1. a flight control system based on wireless telecommunications unmanned plane, including control centre and implementation center, it is characterised in that:
Implementation center includes receiver module, A/D module, trigger, triggering sound wave device, performs module, wherein:
Described receiver module: the instruction receiving control centre is sent to perform module；
Described A/D module: in gathering the region of the circumference 85-105 mile centered by unmanned plane, all animal informations are transferred to control
The computer at center processed；
Described trigger: any foreign object enters in the region of the circumference 5 miles centered by unmanned plane, flip-flop toggle, simultaneously
Issue instructions to trigger sound wave device and the computer of control centre；
Described triggering sound wave device: receive the instruction of trigger and send infrasonic wave；
Described execution module: receive the instruction of implementation center's receiver module and make corresponding actions.
A kind of flight control system based on wireless telecommunications unmanned plane the most according to claim 1, it is characterised in that: described
Trigger is with automatic collision function, and when unmanned plane is less than 1M with obstacle distance, unmanned plane suspends all instructions the most automatically
Return 5 meters to barrier to be further continued for receiving other instructions.
A kind of flight control system based on wireless telecommunications unmanned plane the most according to claim 1, it is characterised in that: described
Control centre and the command encoder of implementation center and decoder all use STC89C51 single-chip microcomputer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610705756.5A CN106094870A (en) | 2016-08-23 | 2016-08-23 | A kind of flight control system based on wireless telecommunications unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610705756.5A CN106094870A (en) | 2016-08-23 | 2016-08-23 | A kind of flight control system based on wireless telecommunications unmanned plane |
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| Publication Number | Publication Date |
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| CN106094870A true CN106094870A (en) | 2016-11-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610705756.5A Pending CN106094870A (en) | 2016-08-23 | 2016-08-23 | A kind of flight control system based on wireless telecommunications unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019134148A1 (en) * | 2018-01-05 | 2019-07-11 | 深圳市大疆创新科技有限公司 | Method and device for controlling unmanned aerial vehicle, and movable platform |
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| US20110144829A1 (en) * | 2009-12-10 | 2011-06-16 | Korea Atomic Energy Research Institute | Countermeasure system for birds |
| CN203435603U (en) * | 2013-08-30 | 2014-02-19 | 西安四环电力监控设备工程有限公司 | Infrasonic wave bird repelling device |
| CN103814887A (en) * | 2014-01-23 | 2014-05-28 | 北京飞旋天行科技有限公司 | Flight bird repellent and flight bird repelling system |
| CN104053358A (en) * | 2011-11-18 | 2014-09-17 | 空中客车运营简化股份公司 | Method and device for scaring birds acoustically, in particular for aircraft |
| US8988230B2 (en) * | 2011-10-25 | 2015-03-24 | Accipiter Radar Technologies Inc. | Device and method for smart, non-habituating, automatic bird deterrent system |
| CN205390157U (en) * | 2016-03-18 | 2016-07-27 | 马春 | Drive bird unmanned aerial vehicle |
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2016
- 2016-08-23 CN CN201610705756.5A patent/CN106094870A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110144829A1 (en) * | 2009-12-10 | 2011-06-16 | Korea Atomic Energy Research Institute | Countermeasure system for birds |
| US8988230B2 (en) * | 2011-10-25 | 2015-03-24 | Accipiter Radar Technologies Inc. | Device and method for smart, non-habituating, automatic bird deterrent system |
| CN104053358A (en) * | 2011-11-18 | 2014-09-17 | 空中客车运营简化股份公司 | Method and device for scaring birds acoustically, in particular for aircraft |
| CN203435603U (en) * | 2013-08-30 | 2014-02-19 | 西安四环电力监控设备工程有限公司 | Infrasonic wave bird repelling device |
| CN103814887A (en) * | 2014-01-23 | 2014-05-28 | 北京飞旋天行科技有限公司 | Flight bird repellent and flight bird repelling system |
| CN205390157U (en) * | 2016-03-18 | 2016-07-27 | 马春 | Drive bird unmanned aerial vehicle |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019134148A1 (en) * | 2018-01-05 | 2019-07-11 | 深圳市大疆创新科技有限公司 | Method and device for controlling unmanned aerial vehicle, and movable platform |
| CN110612496A (en) * | 2018-01-05 | 2019-12-24 | 深圳市大疆创新科技有限公司 | Control method and device for unmanned aerial vehicle and movable platform |
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Application publication date: 20161109 |