CN220935186U - Integrated laser communication terminal - Google Patents
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- CN220935186U CN220935186U CN202321512429.XU CN202321512429U CN220935186U CN 220935186 U CN220935186 U CN 220935186U CN 202321512429 U CN202321512429 U CN 202321512429U CN 220935186 U CN220935186 U CN 220935186U
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Abstract
The utility model provides an integrated laser communication terminal, which comprises: the device comprises a coarse pointing mechanism, a rear light path component, a telescope component, a reflecting mirror component, a locking and releasing mechanism, a star sensor component, a reference prism and an integrated supporting structure; the telescope component is fixedly connected with the integrated supporting structure after being connected with the coarse pointing mechanism, and a grating part of the coarse pointing mechanism is arranged in an inner cavity of the integrated supporting structure; the star sensor assembly is arranged on the integrated supporting structure and completes ground calibration; the locking and releasing mechanism is used for locking the coarse pointing mechanism at the transmitting active section and separating and releasing the coarse pointing mechanism after the track is entered; the reflector component is connected with the coarse pointing mechanism and controls the direction and angle of the reflector; the rear light path component is arranged inside the integrated supporting structure, so that a relatively fixed rotating load is realized, the performance requirements on driving devices such as a two-dimensional pointing motor, a shafting and the like are reduced, the design difficulty is reduced, and the adaptability of the terminal to the mechanical environment is effectively improved.
Description
Technical Field
The utility model relates to the field of wireless laser communication, in particular to an integrated laser communication terminal.
Background
The laser communication terminal is a device for transmitting information by taking a space laser beam as an information carrier, and has the advantages of high communication capacity, strong confidentiality, strong anti-interference capability, small volume weight and the like compared with the traditional microwave communication. The main components of the optical head mainly comprise an optical head and an integrated processing unit, wherein the optical head is a main carrier for realizing the transmission and the reception of space optical signals, is one of core technologies in laser communication and mainly comprises a high-precision coarse pointing mechanism, a telescope component, a rear light path component and the like. The existing optical head layout scheme mostly adopts modularized layout, and has high decoupling degree but causes structural member redundancy, so that the optical head cannot be miniaturized. The traditional high-precision rough pointing mechanism mainly comprises a swinging mirror type, a theodolite type, a kude type, a periscope type and the like, can effectively meet the working requirements under respective scenes, and has the defects of single adaptation scene, insufficient compactness and the like.
The existing laser communication terminal mainly has the following defects: ① The weight and the volume are large, the traditional design method causes that the miniaturization of the laser communication optical head is difficult to realize on the premise of ensuring the performance, the envelope and the quality are larger, the satellite layout is difficult, and the emission cost is higher; ② The material utilization rate is low, and the traditional design method adopts a modularized design, so that decoupling of all groups of components can be realized, but the utilization rate of the structure is greatly reduced, the processing cost is redundant, and the cost performance of the product is not improved; ③ The adaptive scene is few, the restriction is more, for example, the swing mirror type rough pointing mechanism has small volume, low rotation load and good temperature adaptability, but the wide ratio of the pointing mirror is limited, the wide ratio of the pointing mirror can not realize the wide range of pitching angle change, and the wide ratio is difficult to adapt to application scenes such as different-track laser communication, satellite-ground laser communication and the like; the rotation load of the kude type theodolite is too complex, the requirement on a driving mechanism is high, and the application scene of the laser communication terminal is limited; ④ The optical component is larger, so that the envelope of the whole machine is influenced, for example, the periscope type rough pointing mechanism has large pointing range and relatively fixed rotating load, but the whole optical head has larger weight due to the large light-transmitting caliber and the large-size reflectors on two sides; ⑤ The terminal optical head has high mass center position and large rotational inertia, so that the terminal optical head has large height direction dimension and poor installation adaptability to satellites, and is particularly not suitable for flat satellites. Meanwhile, due to the defects of high mass center position of the optical head and the like, the traditional design method has poor mechanical resistance of all groups of components on the optical head, and the emission active section can generate larger dynamic response so as to cause out-of-tolerance product indexes.
Disclosure of utility model
The present utility model has been made in view of the above-mentioned problems, and has as its object to provide an integrated laser communication terminal which overcomes the above-mentioned problems or at least partially solves the above-mentioned problems.
According to an aspect of the present utility model, there is provided an integrated laser communication terminal including: the device comprises a coarse pointing mechanism, a rear light path component, a telescope component, a reflecting mirror component, a locking and releasing mechanism, a star sensor component, a reference prism and an integrated supporting structure;
The telescope component is fixedly connected with the integrated supporting structure after being connected with the coarse pointing mechanism, and a grating part of the coarse pointing mechanism is arranged in an inner cavity of the integrated supporting structure;
The star sensor assembly is arranged on the integrated supporting structure and completes ground calibration;
The locking and releasing mechanism locks the coarse pointing mechanism at the transmitting active section and unlocks and releases the coarse pointing mechanism after entering the track;
the reflector component is connected with the coarse pointing mechanism and used for controlling the direction and the angle of the reflector;
The rear light path component is arranged inside the integrated supporting structure;
the reference prism is disposed outside the integrated support structure.
Optionally, the coarse pointing mechanism specifically includes: azimuth pointing mechanism and elevation pointing mechanism;
The telescope component is connected with the azimuth pointing mechanism and completes performance debugging;
the telescope assembly is integrally arranged in the inner cavity of the azimuth pointing assembly.
Optionally, the mirror assembly specifically includes: azimuth mirror assembly and elevation mirror assembly;
The azimuth reflecting mirror component is connected with the telescope component, and the pitching reflecting mirror component is connected with the pitching pointing mechanism; the pitching reflecting mirror is structurally arranged in the pitching pointing mechanism;
The emission state position of the coarse pointing mechanism is provided with a locking and releasing mechanism;
the azimuth mirror assembly is coupled to the telescope assembly.
Optionally, the rear light path component specifically includes: the device comprises a transmitting collimation assembly, a receiving coupling assembly, a fine tracking assembly, an advanced aiming assembly, a self-calibration assembly, an optical color separation beam splitting assembly, a tracking camera assembly and a rear light path cover;
The fine tracking component is matched with the tracking camera component and is used for finishing fine pointing and finishing terminal chain establishment tracking;
When the signal light is emitted, the light rays sequentially pass through the emission collimation assembly, the advanced aiming assembly, the optical color separation and light splitting assembly, the fine tracking assembly, the pitching reflecting mirror assembly, the telescope assembly and the azimuth reflecting mirror assembly to finish the emission of the signal light;
When receiving signal light, the signal light ray sequentially passes through the azimuth reflecting mirror assembly, the telescope assembly, the pitching reflecting mirror assembly, the fine tracking assembly, the optical color separation and light splitting assembly and the receiving coupling assembly to finish signal light receiving;
during self-calibration, the self-calibration assembly motor drives the shutter to rotate, and the shutter is opened.
Optionally, the optical dichroic beam splitting component specifically includes: color separation films, narrowband filters, and light separation sheets.
Optionally, the tracking camera assembly specifically includes: tracking camera lens, tracking camera.
Optionally, the self-calibration specifically includes: transmitting self-calibration and receiving self-calibration;
The transmission self-calibration process is as follows: the light sequentially passes through the collimation and emission assembly, the advanced aiming assembly and the color separation assembly, and then a part of light passes through the color separation film of the color separation and light splitting assembly and then reaches the pyramid, and after being reflected by the pyramid, the light passes through the narrow-band filter of the color separation and light splitting assembly and the light splitting film and then reaches the fine tracking assembly, so that the self-calibration of emission is completed;
The receiving self-calibration process is as follows: the light passes through the collimation emission component, the advanced aiming component and a small amount of light sequentially, passes through the color separation and splitting component and reaches the pyramid after passing through the color separation and splitting component and passes through the narrow-band filter and the light splitting piece of the color separation and splitting component after being reflected by the pyramid, and reaches the precise tracking component and the receiving coupling component, so that the receiving self calibration is completed.
The utility model provides an integrated laser communication terminal, which comprises: the device comprises a coarse pointing mechanism, a rear light path component, a telescope component, a reflecting mirror component, a locking and releasing mechanism, a star sensor component, a reference prism and an integrated supporting structure; the coarse pointing mechanism, the telescope assembly and the integrated supporting structure are fixedly connected, and a grating part of the coarse pointing mechanism is arranged in an inner cavity of the integrated supporting structure; the star sensor assembly is arranged on the integrated supporting structure and completes ground calibration; the locking and releasing mechanism is used for transmitting the driving section to lock the coarse pointing mechanism and separating and releasing the coarse pointing mechanism after the terminal is in orbit; the reflector component is connected with the coarse pointing mechanism and used for controlling the direction and the angle of the reflector; the rear light path component is arranged in the integrated supporting structure, so that the relative fixation of rotational inertia in the rough tracking process of the laser communication terminal is ensured, the performance requirements on driving devices such as a two-dimensional pointing motor, a shafting and the like are reduced, the design difficulty is reduced, the product adaptability is improved, and the product life is prolonged; the centroid position of the locking state of the laser communication terminal is effectively reduced, and the dynamic response of the terminal product in the transmitting active section is reduced, so that the adaptability of the terminal to the mechanical environment is effectively improved.
The foregoing description is only an overview of the present utility model, and is intended to be implemented in accordance with the teachings of the present utility model in order that the same may be more clearly understood and to make the same and other objects, features and advantages of the present utility model more readily apparent.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings required for the description of the embodiments will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a diagram illustrating an optical head assembly structure of an integrated laser communication terminal according to an embodiment of the present utility model;
fig. 2 is an optical head diagram of an integrated laser communication terminal according to an embodiment of the present utility model;
FIG. 3 is an exploded view of an optical head according to an embodiment of the present utility model;
FIG. 4 is a diagram of a rear light path assembly according to an embodiment of the present utility model;
FIG. 5 is a schematic view of a load-bearing structure according to an embodiment of the present utility model;
Fig. 6 is a schematic diagram of an on-track working zero position according to an embodiment of the present utility model.
Detailed Description
Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.
The terms "comprising" and "having" and any variations thereof in the description embodiments of the utility model and in the claims and drawings are intended to cover a non-exclusive inclusion, such as a series of steps or elements.
The technical scheme of the utility model is further described in detail below with reference to the accompanying drawings and the examples.
As shown in fig. 1 and fig. 3, the optical head of the laser communication terminal mainly comprises a coarse pointing mechanism 1, a rear light path component 2, a telescope component 3, a reflecting mirror component 4, a locking release mechanism 5, a star sensor 6, a reference prism 7 and an integrated supporting structure 8.
As shown in fig. 2, the relationship of light rays transmitted through the various optical elements of the optical head is described.
As shown in fig. 3, the coarse pointing mechanism includes an azimuth pointing mechanism 11 and a pitch pointing mechanism 12.
As shown in fig. 4, the rear light path assembly 2 includes a rear light path housing 21, an emission collimation assembly 22, a receiving coupling assembly 23, a fine tracking assembly 24, a look ahead assembly 25, a self-calibration assembly 26, an optical dichroic beamsplitter assembly 27, a tracking camera assembly 28, an emission collimation hood 29, and a receiving coupling hood 210.
As shown in fig. 3, the mirror assembly 4 includes an azimuth mirror assembly 41, a elevation mirror assembly 42;
during installation, the rough pointing component 1, the telescope component 3, the reflecting mirror component 4 and the rear light path component 2 can be independently installed and adjusted in parallel (the rear light path component 2 is installed on the integrated supporting structure 8 and is installed and adjusted), and the performance test and the environmental test of related components are completed;
After the assembly and adjustment of all the components are completed, the coarse pointing component 4 completes the installation of the azimuth pointing mechanism 41 and the pitching pointing mechanism 42, the telescope component 3 is connected with the azimuth pointing mechanism 11 and completes the performance adjustment, and the whole telescope component 3 is arranged in the inner cavity of the azimuth pointing component 11, so that the compactness and the miniaturization are realized;
The azimuth mirror assembly 41 is connected to the telescope assembly 3 and the elevation mirror assembly 42 is connected to the elevation pointing mechanism 12. The pitch mirror 42 is disposed within the interior cavity of the pitch pointing mechanism 12 to achieve compactness and miniaturization.
The coarse pointing mechanism 1 and the telescope assembly 3 are fixedly connected with the integrated supporting structure 8, and the grating part of the pitching pointing mechanism 42 is arranged in the inner cavity of the integrated supporting structure 8, so that the envelope can be further reduced;
resetting the locking position of the coarse pointing mechanism 1 is completed, a locking release mechanism 5 is installed, and the azimuth mirror 41 is connected with the integrated supporting structure 8;
The star-sensitive component 6 is arranged on the integrated supporting structure 8, and the ground calibration is completed;
Performing heat control and cable arrangement of the whole machine, thereby completing the assembly of the whole machine;
By placing the telescope assembly 3 between the azimuth mirror 41 and the elevation mirror 42 and structurally inside the axis of the azimuth pointing mechanism 11, the axial dimension (defined as the length direction) of the optical telescope is effectively shortened;
The periscope type and the Coder type are combined, so that the azimuth and pitching pointing range of the coarse pointing mechanism can be greatly increased, and the application scene of the laser communication terminal is increased;
The three-way size of the optical head can be effectively shortened by the beam expanding function of the telescope 3 and arranging the pitching reflector 42 in the pitching direction component 12 structurally, so that the height of the optical head can be effectively reduced, the fundamental frequency of the whole machine can be improved, and the mechanical environment adaptability can be improved;
As shown in fig. 5, by using an integrated support structure 8 and placing pitch pointing mechanism 12 motors, gratings, etc. within features 81 of the integrated support structure 8, the optical head width (defined as the width direction) can be effectively shortened;
As shown in fig. 5, by employing an integral support structure 8 and placing the tracking camera assembly 28 within the integral support structure 8 feature 82, the optical head width can be effectively shortened;
as shown in fig. 5, by using an integral support structure 8 and placing the star-sensitive component 6 within the features 83 of the integral support structure 8, the optical head height is effectively reduced;
through the integrated supporting structure 8, the number of structural parts can be effectively reduced by reducing the supporting structure of the coarse pointing mechanism and the supporting structure of the rear light path component, thereby reducing the envelope and the quality of the whole machine and the cost of the whole machine;
By the measures, the envelope and the weight of the optical head of the laser communication terminal can be effectively reduced, so that the extremely light and small-sized laser communication terminal is realized.
The ground transportation and emission active section locks the coarse pointing mechanism 1 through the locking and releasing mechanism 5, so that reliable connection of all positions of the optical head is realized. After the orbit is launched, the locking and releasing mechanism 5 receives a satellite remote control/program control instruction to unlock, so that the release of the movable part is completed, and the azimuth mirror 41 and the pitching mirror 42 are driven by the azimuth pointing mechanism 11 and the pitching pointing mechanism 12 to move to zero positions, as shown in fig. 6.
When a terminal is linked, the azimuth mirror assembly 41 realizes azimuth angle change under the drive of the azimuth pointing mechanism 11, and the pitching mirror assembly 42 realizes pitching angle change under the drive of the pitching pointing mechanism 42, so that coarse pointing is realized;
When the optical head is used for building a chain, beacon light rays sequentially pass through the azimuth reflecting mirror assembly 41, the telescope assembly 3, the pitching reflecting mirror assembly 42, the fine tracking assembly 24, the color separation film, the narrow-band optical filter, the light separation film, the tracking camera lens and the tracking camera, and the fine direction is adjusted by the 24 fine tracking assembly, so that the terminal chain building tracking is completed;
When receiving signal light, the signal light rays sequentially pass through the azimuth reflecting mirror assembly 41, the telescope assembly 3, the pitching reflecting mirror assembly 42, the fine tracking assembly 24, the color separation film, the narrow-band filter, the light separation film and the receiving coupling assembly 23 to finish the signal light receiving;
When the signal light is emitted, the signal light is emitted by the light passing through the collimation emission component 22, the advanced aiming component 25, the color separation film, the fine tracking component 24, the pitching reflecting mirror component 42, the telescope component 3 and the azimuth reflecting mirror component 41 in sequence;
In conclusion, the application has the advantages of compact structure, high material utilization rate, clear decoupling development route and good environmental adaptability, can realize extremely light and small-sized optical heads of the laser communication terminals, and improves the adaptability of products.
The novel overall layout mode realizes the extremely light miniaturization of the laser communication terminal, and reduces the weight and the development difficulty;
In order to realize the light miniaturization of the laser communication terminal on the premise of ensuring the performance of the whole machine, the novel design method of the coarse pointing mechanism and the telescope assembly creatively selects the design scheme of the periscope type and the Cook type combined coarse pointing mechanism, and fully combines the design advantages of large rotation range of the periscope type coarse pointing mechanism, wide adaptation scene, small turning mirror size of the Cook type coarse pointing mechanism and easy realization of light weight. The telescope is arranged between the periscope type rough pointing group azimuth reflecting mirror and the pitching reflecting mirror, and the beam expanding function of the telescope is utilized, so that compared with the traditional periscope type rough pointing mechanism scheme, the size and weight of the pitching reflecting mirror and the corresponding light-transmitting caliber are greatly reduced, and the defect that the periscope type rough pointing mechanism is not easy to realize light weight and miniaturization is effectively avoided. Meanwhile, the rotation load form is basically fixed, so that the defect that the rotation loads of the kude type and the theodolite type are too complex is effectively overcome;
The integrated terminal optical head supporting structure adopts an integrated supporting structure scheme, wherein the coarse pointing mechanism, the rear light path component, the star sensor and the whole machine share one supporting structure on the premise of further guaranteeing decoupling, assembling and adjusting of all the components;
A shutter type high transmit-receive isolation implementation scheme. By adopting the stepping motor to drive the optical trap form, when the terminal needs to be self-calibrated, the stepping motor is driven to rotate, the optical trap structure rotates away from the front of the angular cone reflector, so that self-calibration can be carried out, after calibration is finished, the stepping motor drives the optical trap structure to return to the initial position, and a signal is fed back to the position through the micro switch, the optical trap can effectively avoid the reflection of self-detection light, and therefore, the high receiving and transmitting isolation degree is maintained.
The utility model can effectively reduce the envelope size and weight of the optical head of the laser communication, thereby improving the adaptability to the installation mode on the satellite and reducing the emission cost; the material utilization rate is effectively improved, the number of structural members of the product and the processing difficulty are further reduced, and the processing cost and the processing difficulty are reduced; the application scene of the laser communication terminal is greatly improved, and the laser communication terminal can be suitable for almost all application scenes such as co-track/off-track laser communication, inter-satellite/satellite-ground laser communication and the like; the relative fixation of the rotational inertia in the rough tracking process of the laser communication terminal is ensured, so that the performance requirements on driving devices such as a rough pointing mechanism motor, a shafting and the like are reduced, the design difficulty is reduced, and the product adaptability and the product service life are improved; the centroid position of the locking state of the laser communication terminal is effectively reduced, and the mechanical response of the terminal product in the transmitting active section is reduced, so that the adaptability of the terminal to the mechanical environment is effectively improved.
The beneficial effects are that: the telescope is arranged between the azimuth reflector and the pitching reflector of the periscope type coarse pointing mechanism, the beam expanding function of the telescope is fully utilized, and an integrated supporting structure design thought is adopted, so that the product envelope and the product quality are extremely light and miniaturized on the premise of ensuring the optical and structural performances;
The utilization rate of structural materials is high, the material use efficiency of the integrated supporting structure is improved through an integrated design thought, and the processing cost of the precious composite material is reduced;
The method has wide application scene, and greatly improves the azimuth and pitching pointing range of the coarse pointing mechanism by combining the novel coarse pointing mechanism with the telescope, thereby greatly improving the application range of the laser communication terminal;
The requirements on the driving components are low, and the azimuth and pitching rotation loads are basically consistent, so that the performance requirements on the driving components can be effectively reduced, and the cost reduction and efficiency improvement are realized;
The satellite has good adaptability, reduces the height dimension of the optical head, can be effectively suitable for various satellite installation, can realize almost all the modes of satellite bottom plate installation/side installation and the like, and improves the adaptability to satellites, including remote sensing satellites, communication satellites, navigation satellites, flat satellites, force-bearing barrel satellites, box plate satellites and the like;
The mechanical environment adaptability is good, the height dimension of the optical head is reduced, the fundamental frequency of the optical head is improved, and the risk of coupling the optical terminal and the satellite frequency is reduced, so that the environment adaptability of a laser terminal product is improved;
The cost is low, the number of structural members is greatly reduced, the size of the pitching reflecting mirror is also greatly reduced compared with that of the traditional periscope type telescope, the processing cost of the structural members and the pitching reflecting mirror of the product is reduced, and the cost reduction and synergy are realized.
The foregoing detailed description of the utility model has been presented for purposes of illustration and description, and it should be understood that the utility model is not limited to the particular embodiments disclosed, but is intended to cover all modifications, equivalents, alternatives, and improvements within the spirit and principles of the utility model.
Claims (6)
1. An integrated laser communication terminal, characterized in that the laser communication terminal comprises: the device comprises a coarse pointing mechanism, a rear light path component, a telescope component, a reflecting mirror component, a locking and releasing mechanism, a star sensor component, a reference prism and an integrated supporting structure;
The telescope component is fixedly connected with the integrated supporting structure after being arranged on the coarse pointing mechanism, and a grating part of the coarse pointing mechanism is arranged in an inner cavity of the integrated supporting structure;
The star sensor assembly is arranged on the integrated supporting structure and completes ground calibration;
The locking and releasing mechanism locks the coarse pointing mechanism at the transmitting active section and unlocks and releases the coarse pointing mechanism after entering the track;
the reflector component is connected with the coarse pointing mechanism and used for controlling the direction and the angle of the reflector;
The rear light path component is arranged inside the integrated supporting structure;
the reference prism is arranged outside the integrated supporting structure;
the coarse pointing mechanism specifically comprises: azimuth pointing mechanism and elevation pointing mechanism;
The telescope component is connected with the azimuth pointing mechanism and completes performance debugging;
the telescope assembly is integrally arranged in the inner cavity of the azimuth pointing assembly.
2. An integrated laser communication terminal according to claim 1, characterized in that said mirror assembly comprises in particular: azimuth mirror assembly and elevation mirror assembly;
The azimuth reflecting mirror component is connected with the telescope component, and the pitching reflecting mirror component is connected with the pitching pointing mechanism; the pitching reflecting mirror is structurally arranged in the pitching pointing mechanism;
The emission state position of the coarse pointing mechanism is provided with a locking and releasing mechanism;
the azimuth mirror assembly is coupled to the telescope assembly.
3. The integrated laser communication terminal as claimed in claim 2, wherein the rear optical path assembly specifically comprises: the device comprises a transmitting collimation assembly, a receiving coupling assembly, a fine tracking assembly, an advanced aiming assembly, a self-calibration assembly, an optical color separation beam splitting assembly, a tracking camera assembly and a rear light path cover;
The fine tracking component is matched with the tracking camera component and is used for finishing fine pointing and finishing terminal chain establishment tracking;
When the signal light is emitted, the light rays sequentially pass through the emission collimation assembly, the advanced aiming assembly, the optical color separation and light splitting assembly, the fine tracking assembly, the pitching reflecting mirror assembly, the telescope assembly and the azimuth reflecting mirror assembly to finish the emission of the signal light;
When receiving signal light, the signal light ray sequentially passes through the azimuth reflecting mirror assembly, the telescope assembly, the pitching reflecting mirror assembly, the fine tracking assembly, the optical color separation and light splitting assembly and the receiving coupling assembly to finish signal light receiving;
during self-calibration, the self-calibration assembly motor drives the shutter to rotate, and the shutter is opened.
4. The integrated laser communication terminal as claimed in claim 3, wherein the optical dichroic beam splitting assembly specifically comprises: color separation films, narrowband filters, and light separation sheets.
5. An integrated laser communication terminal as claimed in claim 3, wherein the tracking camera assembly comprises: tracking camera lens, tracking camera.
6. An integrated laser communication terminal according to claim 3, characterized in that said self-calibration comprises in particular: transmitting self-calibration and receiving self-calibration;
The transmission self-calibration process is as follows: the light sequentially passes through the collimation and emission assembly, the advanced aiming assembly and the color separation assembly, and then a part of light passes through the color separation film of the color separation and light splitting assembly and then reaches the pyramid, and after being reflected by the pyramid, the light passes through the narrow-band filter of the color separation and light splitting assembly and the light splitting film and then reaches the fine tracking assembly, so that the self-calibration of emission is completed;
The receiving self-calibration process is as follows: the light passes through the collimation emission component, the advanced aiming component and a part of light passes through the color separation and splitting component color separation piece and then reaches the pyramid, and after being reflected by the pyramid, the light passes through the color separation and splitting component color separation piece and then passes through the color separation and splitting component narrowband filter and the light separation piece and then reaches the fine tracking component and the receiving coupling component, so that the receiving self calibration is completed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321512429.XU CN220935186U (en) | 2023-06-14 | 2023-06-14 | Integrated laser communication terminal |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321512429.XU CN220935186U (en) | 2023-06-14 | 2023-06-14 | Integrated laser communication terminal |
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| Publication Number | Publication Date |
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| CN220935186U true CN220935186U (en) | 2024-05-10 |
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| CN202321512429.XU Active CN220935186U (en) | 2023-06-14 | 2023-06-14 | Integrated laser communication terminal |
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| CN (1) | CN220935186U (en) |
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2023
- 2023-06-14 CN CN202321512429.XU patent/CN220935186U/en active Active
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