CN103529859A - High-altitude balloon height control device - Google Patents
High-altitude balloon height control device Download PDFInfo
- Publication number
- CN103529859A CN103529859A CN201310513132.XA CN201310513132A CN103529859A CN 103529859 A CN103529859 A CN 103529859A CN 201310513132 A CN201310513132 A CN 201310513132A CN 103529859 A CN103529859 A CN 103529859A
- Authority
- CN
- China
- Prior art keywords
- satellite
- balloon
- aerostat
- height
- altitude balloon
- 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.)
- Pending
Links
Images
Landscapes
- Toys (AREA)
Abstract
A high-altitude balloon height control device comprises a guide pipe, a piston, a change gear set, a satellite signal processing unit, a processor, a power supply unit, a micro motor and drive circuit, a satellite receiving antenna, an upper half casing, a lower half casing, a hanging ring, ground receiving control software and the like. According to the device, the problem that the height cannot be controlled after a high-altitude balloon is released is solved. The high-altitude balloon height control device adopts a satellite relay communication technology, so that remote monitoring on the high-altitude balloon height is realized. Discharge of air in the balloon is controlled by controlling closing of the piston and exhaust vents in the guide pipe, so that the size of the balloon is changed, and the high-altitude balloon height is decreased according to a predetermined value.
Description
Technical field
The present invention relates to a kind of aerostat height controller, the height that can be used for all kinds of large-scale aerostats is controlled, feature be quality light, can global location and control, by changing the existing aerostat height of compacting in balloon, reduce.
Background technology
In the situation such as atmospheric exploration and radar calibration, all need a large-scale aerostat to carry a sonde or reflecting target as tracking target.But balloon altitude is malleable and control not, and remote control distance is limited.
Summary of the invention
Aerostat height controller adopts Big Dipper navigation mechanics of communication, according to function, carry out blocking design, by conduit (1), piston (2), gear teeth wheels (3), satellite-signal processing unit (4), processor (5), power supply unit (6), micromachine and driving circuit (7), satellite earth antenna (8), first half shell (9), Lower Half shell (10), link (11) and ground reception control software (12) etc., formed.Aerostat height controller receives locating information and the short message of current system, and by processor decodes, be steering order, control vent port closure control the gas purging in balloon, change in balloon and press, thereby reach reducing of balloon buoyancy, realized balloon altitude reduction.
Accompanying drawing explanation
Fig. 1 is aerostat height controller outside drawing.
Fig. 2 is aerostat height controller structural drawing.
Fig. 3 is aerostat height controller sectional view.
Fig. 4 is aerostat height controller cut-away view.
Fig. 5 is aerostat height controller control flow chart.
Embodiment
Below in conjunction with accompanying drawing, the enforcement of this example is described in further detail.
Be aerostat height controller outside drawing structural representation of the present invention and aerostat height controller structural drawing as depicted in figs. 1 and 2.It is comprised of conduit (1), piston (2), gear teeth wheels (3), satellite-signal processing unit (4), processor (5), power supply unit (6), micromachine and driving circuit (7), satellite earth antenna (8), first half shell (9), Lower Half shell (10), link (11) and ground reception control software (12) etc.
Ground of the present invention receives control software (12) and runs on Big Dipper commander integrated machine system, according to the current locating information of aerostat height controller, send as required and reduce height instruction, relaying is sent to aerostat height controller via satellite.Steering order is comprised of action command code, numeric data code and check information etc., with the form coding of short message, is sent to aerostat height controller.
After aerostat height controller is released with balloon, satellite earth antenna (8) receives Big Dipper satellite signal, be sent to satellite-signal processing unit (4), after amplifying and processing, calculate current locus coordinate and short message information, last processor (5) is decoded into steering order by short message and spatial positional information.As the height in current position coordinates does not produce exhaust instruction lower than the height in present instruction, otherwise, exhaust instruction produced to micromachine and driving circuit (7).
Micromachine of the present invention and driving circuit (7) drive gear teeth wheels (3) rotation, and four vent ports on conduit (1) and piston (2) are overlapped.When pore overlaps completely, motor reaches spacing state, stops operating.Now gas enters the vent port that first half shell is evenly distributed by surrounding and discharges in balloon.Balloon pressure decreased, causes smaller volume, and buoyancy diminishes, and highly decreases.When reducing arrival specified altitude assignment, processor sends out code, micromachine reversion, and stomatal closure, balloon stops exhaust, and balloon is stabilized in specified altitude assignment.
Obviously, those skilled in the art can carry out various changes and modification and not depart from the spirit and scope of the present invention aerostat height controller of the present invention.Like this, if within of the present invention these are changed and modification belongs to the scope of claim of the present invention and equivalent technologies thereof, also intention of the present invention comprises these changes and modification interior.
The present invention practical proof repeatedly, proves its advanced in performance, rational in infrastructure, reliable operation, puts ball a kind of reliable height controller is provided for high-altitude.
Claims (3)
1. an aerostat height controller, comprise conduit, piston, gear teeth wheels, satellite-signal processing unit, processor, power supply unit, micromachine and driving circuit, satellite earth antenna, first half shell, Lower Half shell, link and ground control software, it is characterized in that described satellite earth antenna and satellite-signal processing unit receive ground and control the short message that software transmits by Beidou satellite system; Described processor can be decoded into steering order by short message and locating information; Described conduit, piston, gear teeth wheels and micromachine and driving circuit are controlled pore according to steering order and are opened and closed, and change in balloon and press, thereby change balloon volume, reduce balloon altitude.
2. aerostat height controller according to claim 1, it is characterized in that, described satellite-signal processing unit comprises satellite navigation location and communication module, be not limited to Big Dipper navigator fix and communication module, also comprise the module in other Global Navigation System with satellite navigation location and communication function.
3. aerostat height controller according to claim 1, is characterized in that, described power supply unit can be low temperature lithium battery, can be also the novel energies such as solar cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310513132.XA CN103529859A (en) | 2013-10-28 | 2013-10-28 | High-altitude balloon height control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310513132.XA CN103529859A (en) | 2013-10-28 | 2013-10-28 | High-altitude balloon height control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103529859A true CN103529859A (en) | 2014-01-22 |
Family
ID=49931946
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310513132.XA Pending CN103529859A (en) | 2013-10-28 | 2013-10-28 | High-altitude balloon height control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103529859A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104007769A (en) * | 2014-04-30 | 2014-08-27 | 燕山大学 | Solar tracking control method for calibrating aerostat batteries |
| CN106291758A (en) * | 2016-07-28 | 2017-01-04 | 无锡信大气象传感网科技有限公司 | A kind of pinpoint sounding balloon |
| CN109455289A (en) * | 2018-10-24 | 2019-03-12 | 广州市双气象器材有限公司 | A kind of high-altitude latex translation sounding balloon |
| CN111547224A (en) * | 2020-04-14 | 2020-08-18 | 中国科学院空天信息创新研究院 | Safety control and positioning recovery device and method for high-altitude balloon |
| CN115529997A (en) * | 2022-10-27 | 2022-12-30 | 福建省气象科学研究所 | Artificial rainfall enhancement device and rainfall enhancement control method for sounding balloon carrier |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020072361A1 (en) * | 1999-06-29 | 2002-06-13 | Gerald M. Knoblach | Airborne constellation of communications platforms and method |
| CN102253429A (en) * | 2011-04-28 | 2011-11-23 | 南京大桥机器有限公司 | Full-automatic air sounding equipment |
| CN202712218U (en) * | 2012-06-08 | 2013-01-30 | 中国电子科技集团公司第十八研究所 | Ultrathin flexible crystal silicon solar cell module |
| US20130175391A1 (en) * | 2012-01-09 | 2013-07-11 | Google Inc. | Relative Positioning of Balloons with Altitude Control and Wind Data |
| CN103318381A (en) * | 2013-07-02 | 2013-09-25 | 大连海事大学 | Automatically-movable monitoring buoy and monitoring method thereof |
-
2013
- 2013-10-28 CN CN201310513132.XA patent/CN103529859A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020072361A1 (en) * | 1999-06-29 | 2002-06-13 | Gerald M. Knoblach | Airborne constellation of communications platforms and method |
| CN102253429A (en) * | 2011-04-28 | 2011-11-23 | 南京大桥机器有限公司 | Full-automatic air sounding equipment |
| US20130175391A1 (en) * | 2012-01-09 | 2013-07-11 | Google Inc. | Relative Positioning of Balloons with Altitude Control and Wind Data |
| CN202712218U (en) * | 2012-06-08 | 2013-01-30 | 中国电子科技集团公司第十八研究所 | Ultrathin flexible crystal silicon solar cell module |
| CN103318381A (en) * | 2013-07-02 | 2013-09-25 | 大连海事大学 | Automatically-movable monitoring buoy and monitoring method thereof |
Non-Patent Citations (1)
| Title |
|---|
| 徐梓斌等: "新型电液激振器特性研究", 《中国机械工程》 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104007769A (en) * | 2014-04-30 | 2014-08-27 | 燕山大学 | Solar tracking control method for calibrating aerostat batteries |
| CN104007769B (en) * | 2014-04-30 | 2016-08-24 | 燕山大学 | Aerostat battery is demarcated and is used solar tracking control method |
| CN106291758A (en) * | 2016-07-28 | 2017-01-04 | 无锡信大气象传感网科技有限公司 | A kind of pinpoint sounding balloon |
| CN109455289A (en) * | 2018-10-24 | 2019-03-12 | 广州市双气象器材有限公司 | A kind of high-altitude latex translation sounding balloon |
| CN109455289B (en) * | 2018-10-24 | 2020-06-30 | 广州市双一气象器材有限公司 | High-altitude latex translation sounding balloon |
| CN111547224A (en) * | 2020-04-14 | 2020-08-18 | 中国科学院空天信息创新研究院 | Safety control and positioning recovery device and method for high-altitude balloon |
| CN115529997A (en) * | 2022-10-27 | 2022-12-30 | 福建省气象科学研究所 | Artificial rainfall enhancement device and rainfall enhancement control method for sounding balloon carrier |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103529859A (en) | High-altitude balloon height control device | |
| CN102253429B (en) | Full-automatic air sounding equipment | |
| US20180093750A1 (en) | Puffing propulsion for super pressure balloons | |
| CN205203376U (en) | Rotorcraft unmanned aerial vehicle that can flexiblely descend | |
| CN103532613A (en) | Unmanned aerial vehicle remote task uploading system and method based on big dipper communication | |
| EP3754302A1 (en) | Flight control and navigation integrated machine | |
| CN205982618U (en) | Radar detection device under water | |
| US11923954B1 (en) | Distributing wireless relays to form an ad hoc wireless network | |
| CN110383712A (en) | Communication relay method, relaying flying body, program and recording medium | |
| CN104133483A (en) | Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof | |
| JP2017095079A5 (en) | ||
| CN102331778A (en) | Handheld device and method for controlling unmanned vehicle by utilizing same | |
| CN203102009U (en) | Four rotor aircraft control system based on mobile phone short messages | |
| CN104537731A (en) | A car key capable of remote control of an environment inside a car | |
| CN103792947A (en) | Small rotor flying robot for medical assistance | |
| CN205844900U (en) | A kind of unmanned plane formation control system | |
| CN205581550U (en) | Four miniature rotor unmanned aerial vehicle controlling means | |
| CN103839376A (en) | Accident positioning device | |
| JP2021190951A (en) | System, unmanned aircraft, management device, program and management method | |
| CN111108458A (en) | System and method for controlling an aircraft using lateral propulsion and vertical movement | |
| CN105667746A (en) | Submarine device with escape boat | |
| CN204775012U (en) | Automobile -mounted terminal based on big dipper satellite positioning | |
| CN211979513U (en) | Unmanned aerial vehicle of built-in airborne computer flies accuse module | |
| CN204214587U (en) | A kind of miniaturization high precision rain glass being applied to unmanned plane | |
| CN114397687A (en) | Differential satellite navigation system of carrier-borne unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140122 |