CN106403958A - Unmanned plane aircraft intelligent course indication system - Google Patents
Unmanned plane aircraft intelligent course indication system Download PDFInfo
- Publication number
- CN106403958A CN106403958A CN201610956491.6A CN201610956491A CN106403958A CN 106403958 A CN106403958 A CN 106403958A CN 201610956491 A CN201610956491 A CN 201610956491A CN 106403958 A CN106403958 A CN 106403958A
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- CN
- China
- Prior art keywords
- course
- lamp
- course lamp
- control system
- unmanned plane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 18
- 238000004088 simulation Methods 0.000 claims 1
- 210000003128 head Anatomy 0.000 description 10
- 241000593989 Scardinius erythrophthalmus Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/20—Instruments for performing navigational calculations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The invention discloses an unmanned plane aircraft intelligent course indication system. The unmanned plane aircraft intelligent course indication system comprises a six-rotor unmanned plane body and arms, the six-rotor unmanned plane body comprises a flight control system, a course light control system and an aircraft power supply system, the aircraft power supply system is electrically connected with the flight control system and the course light control system, the flight control system is electrically connected with the course light control system, a first course light, a second course light, a third course light, a fourth course light, a fifth course light and a sixth course light are arranged on the six arms of the six-rotor unmanned plane body respectively, a processor mainboard, a magnetic compass, a triaxial magnetic sensor and an analog to digital converter are arranged in the flight control system, the processor mainboard is electrically connected with the magnetic compass, the triaxial magnetic sensor and the analog to digital converter, and the analog to digital converter is connected with the course light control system. The unmanned plane aircraft intelligent course indication system can accurately display the current orientation of the head of an unmanned plane, avoids misoperation and reduces the hidden safety troubles of unmanned plane flight.
Description
Technical field
The present invention relates to vehicle technology field, particularly to a kind of unmanned plane during flying device intelligence bearing indication system.
Background technology
Existing unmanned plane (many rotors type) is difficult to by naked eyes because its unique resemblance determines its profile
It is more difficult to see aircraft when differentiating heading, particularly flight in the air.Now it is accomplished by using course lamp ancillary terrestrial
Operating personnel recognize to direction.The manned machine (fixed-wing type) of traditional civil aviaton is using left redness on the wing of aircraft
Right green tail three signal lamps of white to aircraft flight state, plane nose towards etc. information be shown.Many rotors then make
Identify its heading with red eye, greensignal light identifies its tail direction.
Content of the invention
The technical problem to be solved is to provide a kind of unmanned plane during flying device intelligence bearing indication system, to solve
The above-mentioned multinomial defect leading in prior art.
For achieving the above object, the present invention provides following technical scheme：A kind of unmanned plane during flying device intelligence bearing indication
System, including six rotor wing unmanned aerial vehicle bodies and horn, this internal inclusion flight control system of six rotor wing unmanned aerial vehicles, course lamp control
System and aircraft electric power system, described aircraft electric power system and flight control system and course lamp control system electrically connect
Connect, described flight control system is electrically connected with course lamp control system, on six horns of described six rotor wing unmanned aerial vehicle bodies
It is respectively equipped with the first course lamp, the second course lamp, the 3rd course lamp, the 4th course lamp, the 5th course lamp and the 6th course lamp, institute
State and in flight control system, be provided with processor main board, magnetic compass, magnetic sensor, analog-digital converter, described processor
Mainboard and magnetic compass, magnetic sensor and analog-digital converter electric connection, described analog-digital converter and course lamp
Control system is connected, described course lamp control system respectively with the first course lamp, the second course lamp, the 3rd course lamp, the 4th
Course lamp, the 5th course lamp, the 6th course lamp are electrically connected with.
Preferably, described first course lamp, the second course lamp, the 3rd course lamp, the 4th course lamp, the 5th course lamp,
It is equipped with red LED lamp and green LED lamp in six course lamps.
Preferably, described aircraft electric power system respectively with the first course lamp, the second course lamp, the 3rd course lamp, the 4th
Course lamp, the 5th course lamp, the 6th course lamp are electrically connected with.
Beneficial effect using above technical scheme is：A kind of present invention unmanned plane during flying device intelligence bearing indication system,
All there is a course lamp below each horn, in each course lamp, be provided with red LED lamp and green LED lamp, and and course
Lamp system is connected, and when aircraft horn is more, instruction is more with course lantern festival, and now head instruction can be more accurate, many rotors
As a example six axle types, course lamp is connected with course lamp control system by holding wire, is aided with the input of aircraft electric power system simultaneously
Power supply, the signal of the true heading of current flight device is passed to course lamp control system by flight control system, according to current
Aircraft is currently true to carry out contrast parsing, final output towards original direction (physics heading) with course lamp control system
Signal controls course lamp, controls course lamp current color by setting, and such as redness represents head, and green represents tail, Qi Tahang
Do not have color or red green two color all bright to lamp, awing, course lamp correctly can indicate heading to such unmanned plane,
Facilitate unmanned plane manipulator to determine unmanned plane heading and flight condition, in some complicated flight environment of vehicle, need to winged
Row device carries out head redirection, and course lamp can go out the direction in currently new course by accurate identification, it is to avoid maloperation, aircraft head
Direction still can wrong will not indicate after redirecting, this mode may avoid flight safety again as traditional approach
Hidden danger, heading can facilitate operating personnel to operate after being explicitly indicated.
Brief description
Fig. 1 is state one structural representation of the present invention；
Fig. 2 is state two structural representation of the present invention；
Fig. 3 is the structured flowchart of the present invention.
Wherein, 1- six rotor wing unmanned aerial vehicle body, 2- horn, 3- flight control system, 4- course lamp control system, 5- flies
Device electric power system, 6- the first course lamp, 7- the second course lamp, 8- the 3rd course lamp, 9- the 4th course lamp, 10- the 5th course lamp,
11- the 6th course lamp, 12- processor main board, 13- magnetic compass, 14- magnetic sensor, 15- analog-digital converter, 16- is red
Color LED, 17- green LED lamp.
Specific embodiment
Describe the preferred embodiment of the present invention below in conjunction with the accompanying drawings in detail.
Fig. 1, Fig. 2 and Fig. 3 show the specific embodiment of the present invention：A kind of unmanned plane during flying device intelligence bearing indication system
System, including six rotor wing unmanned aerial vehicle bodies 1 and horn 2, includes flight control system 3, course lamp control in six rotor wing unmanned aerial vehicle bodies 1
System 4 processed and aircraft electric power system 5, described aircraft electric power system 5 and flight control system 3 and course lamp control system 4
It is electrically connected with, described flight control system 3 and course lamp control system 4 are electrically connected with, the six of described six rotor wing unmanned aerial vehicle bodies 1
First course lamp 6, the second course lamp 7, the 3rd course lamp 8, the 4th course lamp 9, the 5th course lamp 10 are respectively equipped with individual horn 2
With the 6th course lamp 11, in described flight control system 3, it is provided with processor main board 12, magnetic compass 13, magnetic sensor 14, mould
Intend digital quantizer 15, described processor main board 12 and magnetic compass 13, magnetic sensor 14 and analog-digital converter 15 electricity
Property connect, described analog-digital converter 15 is connected with course lamp control system 4, described course lamp control system 4 respectively with
First course lamp 6, the second course lamp 7, the 3rd course lamp 8, the 4th course lamp 9, the 5th course lamp 10, the 6th course lamp 11 are electrical
Connect.
In the present embodiment, described first course lamp 6, the second course lamp 7, the 3rd course lamp 8, the 4th course lamp the 9, the 5th boat
It is equipped with red LED lamp 16 and green LED lamp 17 into lamp 10, the 6th course lamp 11.
In the present embodiment, described aircraft electric power system 5 respectively with the first course lamp 6, the second course lamp 7, the 3rd course
Lamp 8, the 4th course lamp 9, the 5th course lamp 10, the 6th course lamp 11 are electrically connected with.
Unmanned plane axis of orientation angle is total up to 360 °, 0 ° be heading, 180 ° be tail direction, each course lamp according to
Many rotor wing unmanned aerial vehicles horn 2 quantity, the angle that 360 ° of mean allocation, before flight, first set a physics heading, be the
One course lamp 6 and the middle direction of the second course lamp 7, when unmanned plane change of flight direction, the first adjustment angle of meeting, three axle magnetic sensings
Magnetic compass 13 is changed nyctitropic signal transmission to processor main board 12 by device 14, calculates true heading and physics head side
To the angle of change, and the variable signal of angle is passed to course lamp control system 4, course by analog-digital converter 15
Red LED lamp 16 in signal lamp on true head steering wheel arm 2 is lighted by lamp control system 4, such as default first course lamp 6 He
The middle direction of second course lamp 7 is physics heading, when starting to take off, red in the first course lamp 6 and the second course lamp 7
Color LED 16 is bright, and the green LED lamp 17 in the 4th course lamp 9 and the 5th course lamp 10 is bright, represents tail direction, the 3rd course
Lamp 8 and the 6th course lamp 11 does not work or red LED lamp 16 is bright together with green LED lamp 17, when unmanned plane heading changes
Afterwards, the first situation, in horn 2 direction of principal axis, state is just like the red LED lamp in Fig. 1, in the 5th course lamp 10 for heading
16 is bright, represents heading, and the green LED lamp 17 in the second course lamp 7 is bright, represents tail, the first course lamp 6, the 3rd course
Lamp in lamp 8, the 4th course lamp 9, the 6th course lamp 11 does not work.Second situation, heading in the middle of two horns 2, such as
In Fig. 2, when unmanned plane heading is between the first course lamp 6 and the 6th course lamp 11, the first course lamp 6 and the 6th course lamp
Red LED lamp 16 in 11 is bright, represents heading, and the green LED lamp 17 in the 3rd course lamp 8 and the 4th course lamp 9 is bright, generation
Table tail direction, the second course lamp 7 and the 5th course lamp 10 do not work.
Based on above-mentioned：All there is a course lamp below each horn 2, in each course lamp, be provided with red LED lamp 16 He
Green LED lamp 17, and be connected with course lamp system, when aircraft horn more than 2, instruction is more, now with course lantern festival
Head instruction can be more accurate, and as a example many rotor six axle types, course lamp is connected with course lamp control system 4 by holding wire, with
When be aided with aircraft electric power system 5 input power, the signal of the true heading of current flight device is passed by flight control system 3
To course lamp control system 4, according to current flight device currently truly towards original direction (physical machine with course lamp control system 4
Head direction) carry out contrast parsing, final output signal controls course lamp, controls course lamp current color by setting, such as red
Represent head, green represents tail, other courses lamp does not have color or red green two color all bright, such unmanned plane awing,
Course lamp correctly can indicate heading, facilitates unmanned plane manipulator to determine unmanned plane heading and flight condition,
In some complicated flight environment of vehicle, need aircraft is carried out head redirection, course lamp accurate identification can go out and currently newly navigate
To direction, it is to avoid maloperation, aircraft heading will not again as traditional approach, redirect after still can be wrong
Instruction, this mode may avoid flight safety hidden danger, and heading can facilitate operating personnel to operate after being explicitly indicated.
Above-described is only the preferred embodiment of the present invention it is noted that for those of ordinary skill in the art
For, without departing from the concept of the premise of the invention, some deformation can also be made and improve, these broadly fall into the present invention
Protection domain.
Claims (3)
1. a kind of unmanned plane during flying device intelligence bearing indication system, including six rotor wing unmanned aerial vehicle bodies and horn it is characterised in that：
This internal inclusion flight control system of six rotor wing unmanned aerial vehicles, course lamp control system and aircraft electric power system, described aircraft
Electric power system is electrically connected with flight control system and course lamp control system, and described flight control system controls system with course lamp
System be electrically connected with, six horns of described six rotor wing unmanned aerial vehicle bodies are respectively equipped with the first course lamp, the second course lamp, the 3rd
Course lamp, the 4th course lamp, the 5th course lamp and the 6th course lamp, are provided with processor main board, magnetic in described flight control system
Compass, magnetic sensor, analog-digital converter, described processor main board and magnetic compass, magnetic sensor and simulation number
Word converter is electrically connected with, and described analog-digital converter is connected with course lamp control system, described course lamp control system
Electrically connect with the first course lamp, the second course lamp, the 3rd course lamp, the 4th course lamp, the 5th course lamp, the 6th course lamp respectively
Connect.
2. a kind of unmanned plane during flying device intelligence bearing indication system according to claim 1 it is characterised in that：Described first
It is equipped with red LED in course lamp, the second course lamp, the 3rd course lamp, the 4th course lamp, the 5th course lamp, the 6th course lamp
Lamp and green LED lamp.
3. a kind of unmanned plane during flying device intelligence bearing indication system according to claim 1 it is characterised in that：Described flight
Device electric power system respectively with the first course lamp, the second course lamp, the 3rd course lamp, the 4th course lamp, the 5th course lamp, the 6th boat
It is electrically connected with to lamp.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610956491.6A CN106403958B (en) | 2016-10-27 | 2016-10-27 | A kind of unmanned plane during flying device intelligence bearing indication system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610956491.6A CN106403958B (en) | 2016-10-27 | 2016-10-27 | A kind of unmanned plane during flying device intelligence bearing indication system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106403958A true CN106403958A (en) | 2017-02-15 |
| CN106403958B CN106403958B (en) | 2019-04-02 |
Family
ID=58014528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610956491.6A Active CN106403958B (en) | 2016-10-27 | 2016-10-27 | A kind of unmanned plane during flying device intelligence bearing indication system |
Country Status (1)
| Country | Link |
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| CN (1) | CN106403958B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107396491A (en) * | 2017-07-11 | 2017-11-24 | 广东容祺智能科技有限公司 | A kind of course lamp driving of unmanned plane body and control system |
| WO2023207169A1 (en) * | 2022-04-28 | 2023-11-02 | 亿航智能设备（广州）有限公司 | Navigation light system, rotary wing aircraft, and navigation light control system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203047531U (en) * | 2012-11-15 | 2013-07-10 | 深圳市大疆创新科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN204297076U (en) * | 2014-10-16 | 2015-04-29 | 王春辉 | A kind of six axle aircraft |
| CN105346709A (en) * | 2015-11-05 | 2016-02-24 | 广州地理研究所 | Multi-rotor craft capable of transforming combination |
| CN205186545U (en) * | 2015-12-03 | 2016-04-27 | 天津经天航空科技有限公司 | Many rotor unmanned aerial vehicle navigation light indication device |
| CN205524926U (en) * | 2016-01-29 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Lamp shade and use horn structure, unmanned aerial vehicle of this lamp shade |
-
2016
- 2016-10-27 CN CN201610956491.6A patent/CN106403958B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203047531U (en) * | 2012-11-15 | 2013-07-10 | 深圳市大疆创新科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN204297076U (en) * | 2014-10-16 | 2015-04-29 | 王春辉 | A kind of six axle aircraft |
| CN105346709A (en) * | 2015-11-05 | 2016-02-24 | 广州地理研究所 | Multi-rotor craft capable of transforming combination |
| CN205186545U (en) * | 2015-12-03 | 2016-04-27 | 天津经天航空科技有限公司 | Many rotor unmanned aerial vehicle navigation light indication device |
| CN205524926U (en) * | 2016-01-29 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Lamp shade and use horn structure, unmanned aerial vehicle of this lamp shade |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107396491A (en) * | 2017-07-11 | 2017-11-24 | 广东容祺智能科技有限公司 | A kind of course lamp driving of unmanned plane body and control system |
| WO2023207169A1 (en) * | 2022-04-28 | 2023-11-02 | 亿航智能设备（广州）有限公司 | Navigation light system, rotary wing aircraft, and navigation light control system |
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| Publication number | Publication date |
|---|---|
| CN106403958B (en) | 2019-04-02 |
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