CN101183267A - High altitude kite balloon airship control device - Google Patents
High altitude kite balloon airship control device Download PDFInfo
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- CN101183267A CN101183267A CNA2007101912739A CN200710191273A CN101183267A CN 101183267 A CN101183267 A CN 101183267A CN A2007101912739 A CNA2007101912739 A CN A2007101912739A CN 200710191273 A CN200710191273 A CN 200710191273A CN 101183267 A CN101183267 A CN 101183267A
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- chip microcomputer
- high altitude
- empennage
- balloonet
- gasbag
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Abstract
The invention relates to a control device for high altitude mooring boats, comprising a high altitude mooring boat 1. The invention is characterized in that: the high altitude mooring boat is connected with a hanging bin and a mooring rope by a hanger; a front accessory gasbag, a rear accessory gasbag, a flank gasbag and an empennage gasbag are arranged on the high altitude mooring boat; a front valve and a front blower are arranged on the front accessory gasbag; a rear valve and a rear blower are arranged on the rear accessory gasbag; an empennage blower is arranged on the empennage gasbag; a helium valve and the driving motor of the helium valve are arranged on the boat body of the high altitude mooring boat; a tilt sensor and a wind detecting instrument are arranged on the hanger; three pressure sensors are respectively arranged on the front accessory gasbag, the rear accessory gasbag and the empennage gasbag; a single-chip microcomputer, a computer and a temperature sensor are arranged in the hanger. The invention has the advantages of applicability to control of high altitude airships, and high accuracy.
Description
Technical field
The present invention relates to wireless remote control technology and person in electronics, specifically is a kind of high altitude kite balloon airship control device.
Background technology
High altitude kite balloon airship is very universal in the experiment of high-altitude at present, but volume surpasses 4000 cubic metres, lets fly away highly to surpass 5000m seldom, its control device more complicated.
Summary of the invention
The purpose of this invention is to provide a kind of high altitude kite balloon airship control device.
Technical scheme of the present invention is as follows:
High altitude kite balloon airship control device, include high altitude kite balloon airship, high altitude kite balloon airship hangs storehouse and mooring line by the suspension bracket connection, preceding balloonet is arranged on the described high altitude kite balloon airship, back balloonet, the flank air bag, the empennage air bag, it is characterized in that on the described preceding balloonet early gate being installed, preceding fan blower, on the back balloonet late gate is installed, back fan blower, the empennage fan blower is installed on the empennage air bag, helium valve and its drive motor are installed on the hull of high altitude kite balloon airship, inclination sensor and anemometer are installed on the described suspension bracket, before, back balloonet, be separately installed with pressure transducer on the empennage air bag, hang single-chip microcomputer is installed in the storehouse, computing machine and temperature sensor; The output signal of described pressure transducer, inclination sensor, anemometer, temperature sensor is respectively through being linked into the A/D conversion input port of single-chip microcomputer after the low-pass filtering, power supply voltage signal is also sent into the A/D conversion input port of single-chip microcomputer through sending into the A/D conversion input port of inserting single-chip microcomputer behind the voltage follower after the dividing potential drop after other has current signal to amplify through operational amplifier; The output signal of single-chip microcomputer is linked into Darlington transistor, and Darlington transistor is exported control signal respectively and is linked into preceding fan blower, back fan blower, early gate, late gate, empennage fan blower; Have timer to provide work clock for drive motor, single-chip microcomputer output signal is respectively controlled power switch, the helium valve of triode as drive motor; Single-chip microcomputer communicates by differential bus transceiver and computing machine.
The present invention at first simulating signals such as the simulating signal that is installed in inclination sensor on the mooring ship, pressure transducer, temperature sensor, anemometer and electric current, voltages through the A/D conversion of being sent to single-chip microcomputer behind the low-pass filter mouthful, convert to after the digital signal parameters to be dealt into and hang computing machine in the storehouse, hang in the storehouse computing machine then and parameter is beamed back ground-based computer by wireless network by 485 serial ports; Ground-based computer receives after data make analysis and judgement, send steering order to hanging computing machine in the storehouse, hang computing machine in the storehouse and issue single-chip microcomputer in the control enclosure again, balloonet fan blower, back balloonet fan blower, empennage fan blower, preceding balloonet valve, back balloonet valve, helium valve (the helium valve has only when being in an emergency, and just opens when having broken such as mooring line) before controlling by the Single-chip Controlling driving circuit at last.When the ground computing machine when hanging in the storehouse computing machine or hanging that computing machine lost efficacy with single chip communication in the storehouse, the control of each functional circuit of mooring ship is just directly made judgement by single-chip microcomputer according to the sensor signal that collects and is controlled automatically.
Ground-based computer intercoms with computing machine in the storehouse is hung in the high-altitude mutually by wireless network, hangs computing machine in the storehouse and intercoms mutually by the single-chip microcomputer in the control enclosure on 485 serial ports and the suspension bracket.
Description of drawings
Fig. 1 is a mooring ship structural representation.
Fig. 2 is an electrical schematic diagram of the present invention.
Embodiment
Referring to accompanying drawing.
High altitude kite balloon airship control device, include high altitude kite balloon airship 1, high altitude kite balloon airship hangs storehouse and mooring line by the suspension bracket connection, preceding balloonet is arranged on the described high altitude kite balloon airship, back balloonet, flank, the empennage air bag, on the preceding balloonet early gate is installed, preceding fan blower, on the back balloonet late gate is installed, back fan blower, the empennage fan blower is installed on the empennage air bag, helium valve and its drive motor are installed on the hull of high altitude kite balloon airship, inclination sensor and anemometer are installed on the described suspension bracket, before, back balloonet, be separately installed with pressure transducer on the empennage air bag, hang single-chip microcomputer is installed in the storehouse, computing machine and temperature sensor.
U1 is an inclination sensor among Fig. 2; U2 is an operational amplifier; U4 is the PIC16F877A single-chip microcomputer of microchip company; U5 is 555 timers; U6 is the 78L05 three terminal regulator; U7 is RS-485 differential bus transceiver SN65LBC184; U8 is Darlington transistor MC1413; Q1 is large power triode TP127; Wireless bridge adopts U.S. Axelwave carrier class outdoor version wireless bridge; Pressure transducer has adopted three PT201 type pressure units; The anemometer MODEL 05103V WINDMONITOR of U.S. R.M.YOUNG company; Stepper motor adopts Hayden's linear stepping motor.
Behind the RC filter network of the simulating signal of the pressure transducer of preceding balloonet through R1 and C2 composition, send into the crus secunda RA0 mouth of single-chip microcomputer again through the R2 current limliting; Behind the RC filter network of the simulating signal of the pressure transducer of back balloonet through R3 and C3 composition, send into the tripod RA1 mouth of single-chip microcomputer again through the R4 current limliting; Send into the 4th pin RA2 mouth of single-chip microcomputer behind the RC filter network of the simulating signal of the pressure transducer of empennage air bag through R6 and C4 composition again through the R7 current limliting; Send into the 5th pin RA3 mouth of single-chip microcomputer behind the RC filter network of the simulating signal of the wind speed of anemometer output through R8 and C5 composition again through the R9 current limliting; Send into the 6th pin RA5 mouth of single-chip microcomputer behind the RC filter network of the simulating signal of the wind direction of anemometer output through R10 and C6 composition again through the R11 current limliting; Send into the octal RE0 mouth of single-chip microcomputer behind the RC filter network of the simulating signal of inclination sensor through R13 and C8 composition again through the R14 current limliting; Supply voltage is through sending into the 9th pin RE1 mouth of sending into single-chip microcomputer behind the voltage follower that is made of operational amplifier again through the R18 current limliting after R16 and the R19 dividing potential drop; After amplifying through operational amplifier, the current value signal sends into the 10th pin RE2 mouth of single-chip microcomputer again through the R21 current limliting; RA0, RA1, RA2, RA3, RA5, RE0, RE1, RE2 are the A/D conversion input port of single-chip microcomputer.
The 19th pin RD0 mouth with single-chip microcomputer inserts the switch controlling signal of its (MC1413) the seven tunnel of the 7th foot control system of Darlington transistor MC1413 as the preceding fan blower of preceding balloonet through R29; With the 20th pin RD1 mouth of single-chip microcomputer through R30 insert Darlington transistor MC1413 the 6th foot control system it the 6 the tunnel as the back switch controlling signal of the back fan blower of balloonet; Insert its 5 tunnel the control signal of the 5th foot control system of Darlington transistor MC1413 as the early gate of opening preceding balloonet through R31 with the 21st pin RD2 mouth of single-chip microcomputer; Insert its 4 tunnel the control signal of the 4th foot control system of Darlington transistor MC1413 as the early gate of closing preceding balloonet through R32 with the 22nd pin RD3 mouth of single-chip microcomputer; Insert its 3 tunnel the control signal of the 3rd foot control system of Darlington transistor MC1413 as the late gate of opening the back balloonet through R33 with the 27th pin RD4 mouth of single-chip microcomputer; Insert its 2 tunnel the control signal of the 2nd foot control system of Darlington transistor MC1413 as the late gate of closing the back balloonet through R34 with the 28th pin RD5 mouth of single-chip microcomputer; Insert its 1 tunnel the control signal of the 1st foot control system of Darlington transistor MC1413 as the empennage blower switch through R35 with the 29th pin RD6 mouth of single-chip microcomputer.
Do an oscillator with timer NE555 and provide work clock for stepper motor; Control the power switch of Q1 (being large power triode TP127) with the 30th pin RD7 mouth of single-chip microcomputer as stepper motor; J4 is helium valve control delivery outlet.
The 26th pin of single-chip microcomputer is connected with the 1st pin of SN65LBC184, and the 24th pin of single-chip microcomputer is connected as the serial communication line with the 4th pin of SN65LBC184; The 25th pin of single-chip microcomputer is connected the transmitting-receiving control line as serial ports with the 2nd, 3 pin of SN65LBC184; R39 is a build-out resistor; J4 is the communication interface of single-chip microcomputer and computing machine.
Claims (1)
1. high altitude kite balloon airship control device, include high altitude kite balloon airship, high altitude kite balloon airship hangs storehouse and mooring line by the suspension bracket connection, preceding balloonet is arranged on the described high altitude kite balloon airship, back balloonet, the flank air bag, the empennage air bag, it is characterized in that on the described preceding balloonet early gate being installed, preceding fan blower, on the back balloonet late gate is installed, back fan blower, the empennage fan blower is installed on the empennage air bag, helium valve and its drive motor are installed on the hull of high altitude kite balloon airship, inclination sensor and anemometer are installed on the described suspension bracket, before, back balloonet, be separately installed with pressure transducer on the empennage air bag, hang single-chip microcomputer is installed in the storehouse, computing machine and temperature sensor; The output signal of described pressure transducer, inclination sensor, anemometer, temperature sensor is respectively through being linked into the A/D conversion input port of single-chip microcomputer after the low-pass filtering, power supply voltage signal is also sent into the A/D conversion input port of single-chip microcomputer through sending into the A/D conversion input port of inserting single-chip microcomputer behind the voltage follower after the dividing potential drop after other has current signal to amplify through operational amplifier; The output signal of single-chip microcomputer is linked into Darlington transistor, and Darlington transistor is exported control signal respectively and is linked into preceding fan blower, back fan blower, early gate, late gate, empennage fan blower; Have timer to provide work clock for drive motor, single-chip microcomputer output signal is respectively controlled power switch, the helium valve of triode as drive motor; Single-chip microcomputer communicates by differential bus transceiver and computing machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007101912739A CN100498624C (en) | 2007-12-07 | 2007-12-07 | High altitude kite balloon airship control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007101912739A CN100498624C (en) | 2007-12-07 | 2007-12-07 | High altitude kite balloon airship control device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101183267A true CN101183267A (en) | 2008-05-21 |
| CN100498624C CN100498624C (en) | 2009-06-10 |
Family
ID=39448570
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2007101912739A Expired - Fee Related CN100498624C (en) | 2007-12-07 | 2007-12-07 | High altitude kite balloon airship control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100498624C (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102033546A (en) * | 2010-11-09 | 2011-04-27 | 上海交通大学 | Low-altitude airship flight control system and flight control method thereof |
| CN102939239A (en) * | 2010-06-16 | 2013-02-20 | 丹尼尔·S.·瑞德福特 | Airborne elevator apparatus |
| CN102991664A (en) * | 2012-12-03 | 2013-03-27 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN104029812A (en) * | 2014-06-25 | 2014-09-10 | 中国科学院光电研究院 | Electric control valve and stratospheric airship intake and exhaust integrated device |
| CN104386235A (en) * | 2014-11-18 | 2015-03-04 | 厦门大学 | Stratospheric airship with ballast compartments |
| CN104590540A (en) * | 2014-11-13 | 2015-05-06 | 中国特种飞行器研究所 | Novel gasbag for airship |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020130220A1 (en) * | 2001-03-13 | 2002-09-19 | Bob Sparks | Airships having simplied construction and improved maneuverability |
| FR2832976B1 (en) * | 2001-12-05 | 2004-04-16 | Didier Costes | SUSPENDED LOAD AIRSHIP |
| JP2005280438A (en) * | 2004-03-29 | 2005-10-13 | Japan Aerospace Exploration Agency | Pressure managing device of airship |
| CN2820701Y (en) * | 2005-08-16 | 2006-09-27 | 旷天金 | Light unmanned driving airship |
-
2007
- 2007-12-07 CN CNB2007101912739A patent/CN100498624C/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102939239A (en) * | 2010-06-16 | 2013-02-20 | 丹尼尔·S.·瑞德福特 | Airborne elevator apparatus |
| CN102033546A (en) * | 2010-11-09 | 2011-04-27 | 上海交通大学 | Low-altitude airship flight control system and flight control method thereof |
| CN102033546B (en) * | 2010-11-09 | 2013-03-27 | 上海交通大学 | Low-altitude airship flight control system and flight control method thereof |
| CN102991664A (en) * | 2012-12-03 | 2013-03-27 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN102991664B (en) * | 2012-12-03 | 2015-05-13 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN104029812A (en) * | 2014-06-25 | 2014-09-10 | 中国科学院光电研究院 | Electric control valve and stratospheric airship intake and exhaust integrated device |
| CN104029812B (en) * | 2014-06-25 | 2017-01-11 | 中国科学院光电研究院 | Electric control valve and stratospheric airship intake and exhaust integrated device |
| CN104590540A (en) * | 2014-11-13 | 2015-05-06 | 中国特种飞行器研究所 | Novel gasbag for airship |
| CN104386235A (en) * | 2014-11-18 | 2015-03-04 | 厦门大学 | Stratospheric airship with ballast compartments |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100498624C (en) | 2009-06-10 |
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Granted publication date: 20090610 Termination date: 20101207 |