CN206209370U - A kind of satellite launching tower supervising device - Google Patents
A kind of satellite launching tower supervising device Download PDFInfo
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- CN206209370U CN206209370U CN201621185496.5U CN201621185496U CN206209370U CN 206209370 U CN206209370 U CN 206209370U CN 201621185496 U CN201621185496 U CN 201621185496U CN 206209370 U CN206209370 U CN 206209370U
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- supervising device
- satellite
- ultrasonic sensor
- magneto
- launching tower
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Abstract
The utility model discloses a kind of satellite launching tower supervising device, belong to satellite launch field, including the satellite being installed on launching tower, a supervising device is installed on the pylon of the launching tower, supervising device is used to monitor satellite launch state and by receipt signal transmission to command set；Supervising device includes one piece of master control borad, single-chip microcomputer is set on master control borad used as main controller, also include ultrasonic sensor and magneto-dependent sensor, ultrasonic sensor and magneto-dependent sensor are disposed in proximity to satellite one end, whether ultrasonic sensor is used to detect the head of satellite by the ultrasonic sensor, the signal output part connection single-chip microcomputer of ultrasonic sensor.The utility model installs a supervising device at the top of launching tower, a monitoring for launch status, simple structure are effectively carried out to rocket, the people of command set can clearly observe the emission state of rocket, it is very clear for result, just can learn emission state without reusing video monitoring system.
Description
Technical field
The utility model belongs to satellite launch field, and in particular to a kind of satellite launching tower supervising device.
Background technology
During satellite launch, it is commonly installed in launching tower, igniting transmitting is carried out by the support of launching tower.But satellite is taken
It is loaded on rocket, is power drive by rocket, launches.Because overall length is more long, and need towards predetermined
Direction transmitting, the situation of transmitting skew must not occur, therefore in emission process, the situation for rocket launching is particularly weighed
Will.
Therefore, command set often installs a supervising device at the scene, but traditional supervising device is typically all used
Camera is monitored, it is necessary to arrange substantial amounts of equipment component, observes by the naked eye rocket launching lift-off situation.
But the supervising device of this mode, its drawback is, because there is substantial amounts of flue dust at rocket launching scene, causes shooting
The shooting sight line of head is affected, the dust for largely flying upward, and the sight line for causing observation is not fine, and all personnel must
Must concentrate on watching transmitting situation；Even if by the more remote of the position placement of camera, but this way can cause to shoot
Unclear situation.
In addition, traditional monitoring device, cost is high, and affected by environment big, service life is not very long, therefore is used
When also have many weak points.
The content of the invention
The utility model is directed to deficiency of the prior art, there is provided a kind of simple structure, and observation is convenient, feeds back clear, inspection
Survey convenient satellite launching tower supervising device.
The utility model is achieved through the following technical solutions：A kind of satellite launching tower supervising device, including install
In the satellite on launching tower, a supervising device is installed on the pylon of the launching tower, supervising device is used to monitor satellite launch
Receipt signal transmission is simultaneously had a receiver for reception supervising device receipt signal to command set, in command set for state；
Wherein, supervising device includes one piece of master control borad, and master control borad is arranged in protecting box, single-chip microcomputer is set on master control borad and is made
It is main controller, also including ultrasonic sensor and magneto-dependent sensor, ultrasonic sensor and magneto-dependent sensor are arranged at and lean on
Nearly satellite one end, whole supervising device is arranged at the top side of satellite, and ultrasonic sensor is used to detect that the head of satellite to be
It is no to pass through the ultrasonic sensor, the signal output part connection single-chip microcomputer of ultrasonic sensor；
Magneto-dependent sensor, for receiving the magnetic bodies in rocket body, the magnetic bodies triggering magneto sensor in rocket leads to
Cross magneto sensor and detection signal is transferred to single-chip microcomputer, the transmitting situation for detecting rocket body portion；
Supervising device also includes an electric power system, and electric power system is used to be single-chip microcomputer, ultrasonic sensor and magnetosensitive
Sensor power；
The output end of single-chip microcomputer sets a wireless transmitter module, for ultrasonic sensor and magneto-dependent sensor to be returned
The electric signal sent back is transferred to the receiver in command set by the wireless transmitter module, has display rocket hair on receiver
Penetrate the receipt sound signal launcher of situation.
Used as preferred technical scheme, electric power system turns including a battery, one piece of solar panel and one
Circuit board is changed, change-over circuit plate is DC-DC modular converters；
The current output terminal of solar panel connects the DC-DC modular converters, and DC-DC modular converters are by the electricity after conversion
Pressure supplies ultrasonic sensor and magneto-dependent sensor；
Battery connects solar panel, for storing electric energy, solar panel be used for directly to single-chip microcomputer and
Wireless transmitter module is powered.
Used as preferred technical scheme, the receiver in command set includes a wireless receiving module, is monitored for receiving
The electric signal that wireless transmitter module is launched in device, wireless receiving module is supplied by solar panel or municipal power supply
Electricity.
Used as preferred technical scheme, receipt sound signal launcher includes more than one receipt sound, including continuous
The rapid sound of drop-wise or the mitigation sound of continuous drop-wise.
Used as preferred technical scheme, receipt sound signal launcher uses a loudspeaker or two loudspeakers, often
Individual loudspeaker has its corresponding sound receipt.
The beneficial effects of the utility model are：The beneficial effects of the utility model are：The utility model is on the top of launching tower
A supervising device is installed in portion, effectively carries out a monitoring for launch status to rocket, simple structure, and the people of command set can be clear
Observe rocket emission state, it is very clear for result, just can learn emitting shape without reusing video monitoring system
State.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is system block diagram of the present utility model.
Specific embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine by any way.
This specification（Including any accessory claim, summary and accompanying drawing）Disclosed in any feature, except non-specifically is chatted
State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature
It is an example in a series of equivalent or similar characteristics.
Including the satellite being installed on launching tower, a supervising device, supervising device are installed on the pylon of the launching tower
For monitoring satellite launch state and by receipt signal transmission to command set, there is a reception supervising device receipt in command set
The receiver of signal；
Supervising device is installed on launching tower upper end, when in the rocket uphill process for being equipped with satellite, enters into supervising device
Monitoring range within after, you can trigger the supervising device, the supervising device after being triggered can in the lump return these receipt signals
It is transmitted to command set.
Supervising device includes one piece of master control borad, and control mainboard needs to be placed in a box body for safety, it is ensured that whole
Circuit part is not attacked by external environment condition, such as extraneous rainwater, mist etc., therefore master control borad is arranged at into guarantor in the present embodiment
In shield box；In order to be dealt with to receipt signal, a single-chip microcomputer can be set on master control borad, used as the treatment of signal receipt
Device；
And it is used to receive the element of signal, it is respectively ultrasonic sensors from two in the present embodiment and magnetosensitive is passed
Sensor, ultrasonic sensor and magneto-dependent sensor are disposed in proximity to satellite one end, in order to set more rationally, supersonic sensing
Device is preferably arranged at the lower end of magneto-dependent sensor so that rising the rocket head for coming can first trigger ultrasonic sensor, then,
The rocket body portion for rising therewith can trigger magneto-dependent sensor；Ultrasonic sensor is used to detect whether the head of satellite passes through
The ultrasonic sensor, after ultrasonic sensor receives the rising receipt signal of rocket head, and the receipt signal transmission is given
Single-chip microcomputer, single-chip microcomputer is by the electric signal transmission to command set.
The use of ultrasonic sensor is applied to more field than wide, and its operation principle is also very simple, ultrasound
Wave sensor launches ultrasonic wave, after running into the rocket of rising, i.e. obstruction, and the ultrasonic wave receipt signal is just reflected, with this
Feedback signal is obtained, ultrasonic sensor will pass to control assembly after receiving the signal for reflecting, inspection is completed with this
Survey, because the use of ultrasonic sensor is relatively common, be not described in detail herein.
Magneto-dependent sensor, for receiving the magnetic bodies in rocket body, the magnetic bodies triggering magneto sensor in rocket leads to
Cross magneto sensor and detection signal is transferred to single-chip microcomputer, the transmitting situation for detecting rocket body portion；
Because rocket is internally provided with magnetic object, therefore, when rocket body is risen at magneto-dependent sensor position, magnetosensitive
Sensor detects magnet and is close to, and magnet-sensitive switch magnetic red piece closure, circuit is connected, and magneto-dependent sensor is obtained and exports electric signal,
To single-chip microcomputer, single-chip microcomputer drives wireless transmitter module by its electric signal transmission to reception to the electric signal transmission after making signal transacting
Device.
The principle of magneto-dependent sensor is relatively common, and the field for using is not described in detail herein also than wide.
Supervising device also includes an electric power system, and electric power system is used to be single-chip microcomputer, ultrasonic sensor and magnetosensitive
Sensor power；
The output end of single-chip microcomputer sets a wireless transmitter module, for ultrasonic sensor and magneto-dependent sensor to be returned
The electric signal sent back is transferred to the receiver in command set by the wireless transmitter module, has display rocket hair on receiver
Penetrate the receipt sound signal launcher of situation.
In order to save electric energy, and because supervising device is arranged on launching tower, height is higher, therefore by electric power system
It is arranged to energy saving and environment friendly solar electric power supply system, therefore, the electric power system includes battery, one piece of solar cell
Plate and a change-over circuit plate, change-over circuit plate are DC-DC modular converters；
The current output terminal of solar panel connects the DC-DC modular converters, and DC-DC modular converters are by the electricity after conversion
Pressure supplies ultrasonic sensor and magneto-dependent sensor；DC-DC modular converters are used for conversion solar cell plate output end voltage, are
Can be used for ultrasonic sensor and magneto-dependent sensor.
Battery connects solar panel, for storing electric energy, solar panel be used for directly to single-chip microcomputer and
Wireless transmitter module is powered, and when not having the sun, battery as the stand-by equipment of electric power, therefore can may also set up on battery
Charging system, except solar charging electrically in addition to, should also have other charging modes, in case of need.
Battery may be disposed in protecting box as control panel, prevent extraneous rainwater from drenching battery or control.
Receiver in command set includes a wireless receiving module, for receiving wireless transmitter module hair in supervising device
Incoming electric signal, wireless receiving module is powered by solar panel or municipal power supply, and the receiver can be positioned over
It is independently arranged in one box body, can go out carrying, can be also accessed in being used together with other monitoring devices.
Receipt sound signal launcher includes more than one receipt sound, including continuous drop-wise rapid sound or continuous
The mitigation sound of drop-wise, works as satellite（Prosthese）During near ultrasonic sensor, whole monitoring device send it is rapid " dichloro-diphenyl-dichlorothane " sound,
At the same time, the receiver in command set also send it is rapid " dichloro-diphenyl-dichlorothane " sound, show the satellite for monitoring in movement, with this table
Show that rocket launching is normal.
When rocket body rises, close to after magneto-dependent sensor, monitoring device can send mitigation " drop drop to internal magnetic bodies
Drop " sound, at the same time, the receiver in command set also send mitigation " dichloro-diphenyl-dichlorothane " sound.Show the rocket for monitoring in movement,
Represent that rocket launching is normal with this.
Receipt sound signal launcher uses a loudspeaker or two loudspeakers, and each loudspeaker is corresponding with its
Sound receipt.
The beneficial effects of the utility model are：The beneficial effects of the utility model are：The utility model is on the top of launching tower
A supervising device is installed in portion, effectively carries out a monitoring for launch status to rocket, simple structure, and the people of command set can be clear
Observe rocket emission state, it is very clear for result, just can learn emitting shape without reusing video monitoring system
State.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Therefore, protection domain of the present utility model should be determined by the scope of protection defined in the claims.
Claims (5)
1. a kind of satellite launching tower supervising device, it is characterised in that：Including the satellite being installed on launching tower, in the launching tower
One supervising device is installed, supervising device is used to monitor satellite launch state and by receipt signal transmission to command set on pylon,
There is a receiver for reception supervising device receipt signal in command set；
Wherein, supervising device includes one piece of master control borad, and master control borad is arranged in protecting box, and single-chip microcomputer is set on master control borad as master
Control device, also including ultrasonic sensor and magneto-dependent sensor, ultrasonic sensor and magneto-dependent sensor are disposed in proximity to defend
Star one end, whole supervising device is arranged at the top side of satellite, and ultrasonic sensor is used to detect whether the head of satellite passes through
Cross the ultrasonic sensor, the signal output part connection single-chip microcomputer of ultrasonic sensor；
Magneto-dependent sensor, for receiving the magnetic bodies in rocket body, the magnetic bodies triggering magneto sensor in rocket, by magnetic
Detection signal is transferred to single-chip microcomputer by quick element, the transmitting situation for detecting rocket body portion；
Supervising device also includes an electric power system, and electric power system is used to be single-chip microcomputer, ultrasonic sensor and magnetosensitive sensing
Device is powered；
The output end of single-chip microcomputer sets a wireless transmitter module, for ultrasonic sensor and magneto-dependent sensor to be returned back
The electric signal for coming is transferred to the receiver in command set by the wireless transmitter module, has display rocket launching feelings on receiver
The receipt sound signal launcher of condition.
2. satellite launching tower supervising device as claimed in claim 1, it is characterised in that：Electric power system include battery,
One piece of solar panel and a change-over circuit plate, change-over circuit plate are DC-DC modular converters；
The current output terminal of solar panel connects the DC-DC modular converters, and DC-DC modular converters supply the voltage after conversion
Ultrasonic sensor and magneto-dependent sensor；
Battery connects solar panel, and for storing electric energy, solar panel is for directly to single-chip microcomputer and wirelessly
Transmitter module is powered.
3. satellite launching tower supervising device as claimed in claim 1, it is characterised in that：Receiver in command set includes one
Wireless receiving module, for receiving the electric signal that wireless transmitter module in supervising device is launched, wireless receiving module passes through
Solar panel or municipal power supply are powered.
4. satellite launching tower supervising device as claimed in claim 1, it is characterised in that：Receipt sound signal launcher includes one
The receipt sound of kind of the above, including continuous drop-wise rapid sound or the mitigation sound of continuous drop-wise.
5. the satellite launching tower supervising device as described in claim 1 or 4, it is characterised in that：Receipt sound signal launcher is adopted
With a loudspeaker or two loudspeakers, each loudspeaker is with its corresponding sound receipt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621185496.5U CN206209370U (en) | 2016-11-04 | 2016-11-04 | A kind of satellite launching tower supervising device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621185496.5U CN206209370U (en) | 2016-11-04 | 2016-11-04 | A kind of satellite launching tower supervising device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206209370U true CN206209370U (en) | 2017-05-31 |
Family
ID=58756839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621185496.5U Active CN206209370U (en) | 2016-11-04 | 2016-11-04 | A kind of satellite launching tower supervising device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206209370U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109725581A (en) * | 2019-01-22 | 2019-05-07 | 北京电子工程总体研究所 | A kind of Intelligent unattended launch control system based on 4G technology |
| WO2021072826A1 (en) * | 2019-10-14 | 2021-04-22 | 唐山维数科技有限公司 | Launching device for simulating rocket launching |
| CN117278734A (en) * | 2023-11-21 | 2023-12-22 | 北京星河动力装备科技有限公司 | Rocket launching immersive viewing system |
-
2016
- 2016-11-04 CN CN201621185496.5U patent/CN206209370U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109725581A (en) * | 2019-01-22 | 2019-05-07 | 北京电子工程总体研究所 | A kind of Intelligent unattended launch control system based on 4G technology |
| CN109725581B (en) * | 2019-01-22 | 2020-09-18 | 北京电子工程总体研究所 | Intelligent unmanned emission control system based on 4G technology |
| WO2021072826A1 (en) * | 2019-10-14 | 2021-04-22 | 唐山维数科技有限公司 | Launching device for simulating rocket launching |
| CN117278734A (en) * | 2023-11-21 | 2023-12-22 | 北京星河动力装备科技有限公司 | Rocket launching immersive viewing system |
| CN117278734B (en) * | 2023-11-21 | 2024-04-19 | 北京星河动力装备科技有限公司 | Rocket launching immersive viewing system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171222 Address after: 518000 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A (located in Shenzhen Qianhai Business Secretary limited) (Shenzhen premises Nanshan District high tech Park South Hing a Hong Kong Polytech University No. 18 building 401, 404, and 406, 407, 408) Patentee after: Hua De en Education Technology Development Co., Ltd. Address before: 518000 Guangdong city of Shenzhen province Nanshan District high tech Industrial Park South Hing a Hong Kong Polytech University No. 18 building 4 Room 408 research Patentee before: Shenzhen Huade Grace Education Information Consulting Co. Ltd. |
|
| TR01 | Transfer of patent right |