CN203190896U - Civil rocket projectile with locating function - Google Patents
Civil rocket projectile with locating function Download PDFInfo
- Publication number
- CN203190896U CN203190896U CN 201320208710 CN201320208710U CN203190896U CN 203190896 U CN203190896 U CN 203190896U CN 201320208710 CN201320208710 CN 201320208710 CN 201320208710 U CN201320208710 U CN 201320208710U CN 203190896 U CN203190896 U CN 203190896U
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- positioning
- civil rocket
- civil
- rocket projectile
- module
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Abstract
The utility model relates to a civil rocket projectile with a locating function, and belongs to the technical field of civil rocket projectiles. The civil rocket projectile comprises a stud, a dissemination device, an engine, a stabilizing device and a locating communication module, wherein a GPS locating module and a wireless communication module are connected with each other through a data wire and then packaged through a shell to form the locating communication module, the locating communication module is arranged inside the stud, and the locating communication module and the stud are separated through foaming material. The civil rocket projectile is simple in structure and convenient to install, resolves the problem that an existing civil rocket projectile can not effectively track a trajectory of the existing civil rocket projectile, and makes a control platform master position information of the civil rocket projectile in real time.
Description
Technical field
The utility model relates to a kind of civil rocket bullet with positioning function, belongs to civil rocket bullet technical field.
Background technology
Existing civil rocket bullet such as hail-proof rain-increasing rocket etc. are uncontrolled missile, rocket projectile after finishing artificial rain operation, by high-altitude parachute-opening freely falling body to ground.Whether the control platform need be collected the rocket projectile ballistic trajectory, normal by the work of ballistic trajectory criterion rocket, and the rocket projectile remains are reclaimed.
Conventional method adopts the mode of radar tracking, civil rocket bullet is in-flight carried out real-time tracking, but the civil rocket bullet is for reducing cost of manufacture, the body majority is nonmetallic materials, its trajectory can not effectively be followed the tracks of and describe to radar, whether can't by ballistic trajectory criterion rocket work normal, and can't determine a rocket projectile remains landing point position if causing, increase recovery difficult.
The utility model content
The purpose of this utility model is can not effectively follow the tracks of the problem of its trajectory in order to solve existing civil rocket bullet, and a kind of civil rocket bullet with positioning function is provided.
The purpose of this utility model is achieved through the following technical solutions:
A kind of civil rocket bullet with positioning function of the present utility model comprises a spiral shell, seeding device, engine, stabilising arrangement, also comprises the positioning and communicating module;
The positioning and communicating module is that the GPS locating module is connected the back casing encapsulation with wireless communication module by data wire;
The positioning and communicating module is installed in the spiral shell, and isolates by expanded material between positioning and communicating module and the spiral shell.
Be fixed on positioning and communicating module in the spiral shell GPS locating module reception antenna stretch out direction, be adjusted to that to flick the umbrella direction consistent with civil rocket, be conducive to strengthen GPS locating module satellite searching ability.
The course of work
After the work of civil rocket bullet, the GPS locating module is the positional information of real-time collecting rocket projectile via satellite, and this positional information is transferred to wireless communication module, wireless communication module is given the control platform with the positional information real-time Transmission of collecting, and makes the control platform grasp the positional information of rocket projectile in real time.
Beneficial effect
The utility model is simple in structure, and is easy for installation, solved the problem that existing civil rocket bullet can not effectively be followed the tracks of its trajectory, makes the control platform grasp the positional information of rocket projectile in real time.
Description of drawings
Fig. 1 is the positioning and communicating module scheme of installation of the utility model civil rocket bullet;
Wherein, 1-spiral shell; The 2-expanded material; 3-positioning and communicating module.
The specific embodiment
Below in conjunction with drawings and Examples content of the present utility model is further described:
Embodiment
A kind of civil rocket bullet with positioning function of the present utility model as shown in Figure 1, comprises a spiral shell 1, seeding device, engine, stabilising arrangement, also comprises positioning and communicating module 3;
The positioning and communicating module is that the GPS locating module is connected the back casing encapsulation with wireless communication module by data wire;
The positioning and communicating module is installed in the spiral shell, and isolates by expanded material 2 between positioning and communicating module and the spiral shell.
Be fixed on positioning and communicating module in the spiral shell GPS locating module reception antenna stretch out direction, be adjusted to that to flick the umbrella direction consistent with civil rocket, be conducive to strengthen GPS locating module satellite searching ability.
After the work of civil rocket bullet, the GPS locating module is the positional information of real-time collecting rocket projectile via satellite, and this positional information is transferred to wireless communication module, wireless communication module is given the control platform with the positional information real-time Transmission of collecting, and makes the control platform grasp the positional information of rocket projectile in real time.
Claims (2)
1. the civil rocket bullet with positioning function comprises a spiral shell, seeding device, engine, stabilising arrangement, it is characterized in that: also comprise the positioning and communicating module;
The positioning and communicating module is that the GPS locating module is connected the back casing encapsulation with wireless communication module by data wire; The positioning and communicating module is installed in the spiral shell, and isolates by expanded material between positioning and communicating module and the spiral shell.
2. a kind of civil rocket bullet with positioning function as claimed in claim 1 is characterized in that: will be fixed on positioning and communicating module in the spiral shell GPS locating module reception antenna stretch out direction, be adjusted to that to flick the umbrella direction consistent with civil rocket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320208710 CN203190896U (en) | 2013-04-24 | 2013-04-24 | Civil rocket projectile with locating function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320208710 CN203190896U (en) | 2013-04-24 | 2013-04-24 | Civil rocket projectile with locating function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203190896U true CN203190896U (en) | 2013-09-11 |
Family
ID=49107749
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320208710 Expired - Fee Related CN203190896U (en) | 2013-04-24 | 2013-04-24 | Civil rocket projectile with locating function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203190896U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN104990465A (en) * | 2015-07-21 | 2015-10-21 | 胡校峰 | Tracking reconnaissance locator and missile having locator |
| CN110231641A (en) * | 2019-07-05 | 2019-09-13 | 上海埃依斯航天科技有限公司 | A kind of rocket one sub grade remains accurate positioning device and localization method |
-
2013
- 2013-04-24 CN CN 201320208710 patent/CN203190896U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN104266555B (en) * | 2014-09-30 | 2017-02-15 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN104990465A (en) * | 2015-07-21 | 2015-10-21 | 胡校峰 | Tracking reconnaissance locator and missile having locator |
| CN110231641A (en) * | 2019-07-05 | 2019-09-13 | 上海埃依斯航天科技有限公司 | A kind of rocket one sub grade remains accurate positioning device and localization method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130911 Termination date: 20160424 |