Intelligent monitoring device for precise orbit flight of microsatellite

Abstract

The utility model discloses an intelligent monitoring device for precise orbit flight of a microsatellite, which is characterized in that the upper end of a bottom column is provided with a lifting assembly, the upper end of the lifting assembly is fixedly connected with a supporting column, the upper end of the supporting column is fixedly connected with a bearing plate, the upper surface of the bearing plate is fixedly connected with a monitoring device body, and the bearing plate is provided with a through hole; a first sliding rod is slidably connected to the inner surface of the through hole, a connecting plate is fixedly connected to the other end of the first sliding rod, a mounting hole is formed in the bearing plate, an electric push rod is fixedly connected to the inner surface of the mounting hole, and the other end of the electric push rod is fixedly connected to the rear surface of the connecting plate. When the device is in a standby state, the protective shell can be moved to provide physical protection, the collision resistance is remarkably improved, meanwhile, a brush and a spray head in the protective shell can effectively clean dust on the surface of the device, the monitoring accuracy is ensured, and therefore the reliability of monitoring data is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of monitoring devices, and particularly relates to an intelligent monitoring device for precise orbital flight of a microsatellite. Background Art

[0002] The existing intelligent monitoring device for precise orbital flight of a microsatellite is usually used to monitor and track the orbital state of a satellite, ensure its flight on a predetermined orbit, and timely adjust the orbit to cope with various external factors. It can improve the safety and effectiveness of satellite operation and provide real-time data for the ground control center.

[0003] However, when it is in use, it does not have physical protection and cleaning components and may face the following problems: vulnerable to damage: lacking physical protection, the device is more likely to be damaged when suffering external impacts, reducing the anti-collision ability; device panel pollution: the accumulation of dust and dirt on the device panel may affect the monitoring effect, resulting in inaccurate or unreliable monitoring data. Summary of the Utility Model

[0004] The purpose of the utility model is to solve at least one of the technical problems existing in the prior art, and provide an intelligent monitoring device for precise orbital flight of a microsatellite. When the device is on standby, the sliding rod one can drive the protective shell to move above the monitoring device body to provide physical protection for the device, reduce the direct impact of external object impacts on the monitoring device body, and improve the anti-collision ability. The dust on the surface of the monitoring device body can be cleaned by the brush inside the protective shell, and the dust can be blown away by the nozzle, so as to achieve the self-cleaning function of the device, keep the device clean, reduce detection errors, and improve the accuracy and reliability of monitoring data.

[0005] The utility model also provides an intelligent monitoring device for precise orbital flight of a microsatellite as described above, including: a bottom plate, the upper surface of the bottom plate is fixedly connected with bottom columns, a lifting component is arranged at the upper end of the bottom columns, the upper end of the lifting component is fixedly connected with a support column, the upper end of the support column is fixedly connected with a bearing plate, the upper surface of the bearing plate is fixedly connected with a monitoring device body, through holes are arranged on the bearing plate, the inner surface of the through holes is slidably connected with a sliding rod one, the other end of the sliding rod one is fixedly connected with a connecting plate, mounting holes are arranged on the bearing plate, the inner surface of the mounting holes is fixedly connected with an electric push rod, the other end of the electric push rod is fixedly connected to the rear surface of the connecting plate, the upper surface of the connecting plate is fixedly connected with a protective shell, the inner surface of the protective shell is rotatably connected with a brush, the brush is movably connected with the monitoring device body, a motor is fixedly connected to the upper surface of the protective shell, the brush is driven by the motor, a nozzle is fixedly connected to the inner surface of the protective shell, an air pump is fixedly connected to the upper surface of the protective shell, the output end of the air pump is communicated with a connecting pipe, and the side surface of the connecting pipe is communicated with the nozzle.

[0006] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein the lifting assembly comprises: a hydraulic cylinder and a hydraulic rod. The hydraulic cylinder is fixedly connected to the upper end of the bottom column, the hydraulic rod is fixedly connected to the output end of the hydraulic cylinder, and the support column is fixedly connected to the upper end of the hydraulic rod.

[0007] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein a lower fixing plate is fixedly connected to the side surface of the bottom column, and a sleeve is fixedly connected to the upper surface of the lower fixing plate.

[0008] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein an upper fixing plate is fixedly connected to the side surface of the support column, a second sliding rod is fixedly connected to the lower surface of the upper fixing plate, and the second sliding rod penetrates to the lower surface of the sleeve.

[0009] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein a limiting plate is fixedly connected to the lower end of the second sliding rod, and the limiting plate is slidably connected to the lower fixing plate.

[0010] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein a side plate is fixedly connected to the side surface of the support column, and a warning light is fixedly connected to the side surface of the side plate.

[0011] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein a fixing hole is fixedly connected to the bottom plate, and a ground nail is movably connected inside the fixing hole.

[0012] An intelligent monitoring device for precise orbital flight of a microsatellite according to the present utility model, wherein a cover shell is fixedly connected to the upper surface of the protective shell, and the motor is located inside the cover shell.

[0013] Advantageous Effects

[0014] 1. Compared with the prior art, when the intelligent monitoring device for precise orbital flight of the microsatellite is on standby, the protective shell can be driven by the first sliding rod to move above the monitoring device body, providing physical protection for the device, reducing the direct impact of external object impacts on the monitoring device body, improving the anti-collision ability. The dust on the surface of the monitoring device body can be cleaned by the brush inside the protective shell, and the dust can be blown away by the nozzle, thus realizing the self-cleaning function of the device, keeping the equipment clean, reducing detection errors, and improving the accuracy and reliability of monitoring data. Description of the Drawings

[0015] The present utility model will be further described below in conjunction with the drawings and embodiments;

[0016] Figure 1 The front view structural diagram of the intelligent monitoring device for precise orbital flight of the micro-satellite of the present utility model;

[0017] Figure 2 The right view sectional structural diagram of the intelligent monitoring device for precise orbital flight of the micro-satellite of the present utility model;

[0018] Figure 3 The left view sectional structural diagram of the intelligent monitoring device for precise orbital flight of the micro-satellite of the present utility model;

[0019] Figure 4 The right view structural diagram of the intelligent monitoring device for precise orbital flight of the micro-satellite of the present utility model.

[0020] Legend description:

[0021] 1. Motor; 2. Housing; 3. First slide bar; 4. Bearing plate; 5. Warning light; 6. Side plate; 7. Upper fixing plate; 8. Sleeve; 9. Second slide bar; 10. Limiting plate; 11. Ground nail; 12. Fixing hole; 13. Connecting pipe; 14. Air pump; 15. Protective shell; 16. Connecting plate; 17. Support column; 18. Hydraulic rod; 19. Hydraulic cylinder; 20. Lower fixing plate; 21. Bottom column; 22. Bottom plate; 23. Sprayer; 24. Brush; 25. Monitoring device body; 26. Electric push rod; 27. Through hole. Specific implementation manners

[0022] This part will describe in detail the specific embodiments of the present utility model. The preferred embodiments of the present utility model are shown in the drawings. The function of the drawings is to supplement the description of the text part of the specification, enabling people to visually and vividly understand each technical feature and the overall technical solution of the present utility model, but it should not be construed as a limitation on the protection scope of the present utility model.

[0023] Referring to Figures 1-4 , an intelligent monitoring device for precise orbital flight of a micro-satellite in an embodiment of the present utility model includes: a bottom plate 22, a bottom column 21 fixedly connected to the upper surface of the bottom plate 22, a fixing hole 12 fixedly connected to the bottom plate 22, a ground nail 11 movably connected inside the fixing hole 12, the bottom column 21 for bottom support, a lower fixing plate 20 fixedly connected to the side surface of the bottom column 21, a sleeve 8 fixedly connected to the upper surface of the lower fixing plate 20, an upper fixing plate 7 fixedly connected to the side surface of a support column 17, a second slide bar 9 fixedly connected to the lower surface of the upper fixing plate 7, the second slide bar 9 penetrating to the lower surface of the sleeve 8, a limiting plate 10 fixedly connected to the lower end of the second slide bar 9, the limiting plate 10 being slidably connected to the lower fixing plate 20, a side plate 6 fixedly connected to the side surface of the support column 17, a warning light 5 fixedly connected to the side surface of the side plate 6, and a lifting assembly provided at the upper end of the bottom column 21 for adjusting the height.

[0024] The lifting assembly includes: a hydraulic cylinder 19 and a hydraulic rod 18. The hydraulic cylinder 19 is fixedly connected to the upper end of the bottom column 21, and the hydraulic rod 18 is fixedly connected to the output end of the hydraulic cylinder 19. A support column 17 is fixedly connected to the upper end of the hydraulic rod 18. The upper end of the lifting assembly is fixedly connected with a support column 17 for supporting and connecting the bearing plate 4. The upper end of the support column 17 is fixedly connected with a bearing plate 4 for connecting the monitoring device body 25. The upper surface of the bearing plate 4 is fixedly connected with the monitoring device body 25, which is an orbital monitor for microsatellites and is a mature existing technology and will not be elaborated in this document. A through hole 27 is provided on the bearing plate 4 for connecting the first slide bar 3. The inner surface of the through hole 27 is slidably connected with the first slide bar 3 for driving the housing 15 to move. The other end of the first slide bar 3 is fixedly connected with a connecting plate 16 for connecting the housing 15. An installation hole is provided on the bearing plate 4, and the inner surface of the installation hole is fixedly connected with an electric push rod 26 for driving the connecting plate 16 to move. The other end of the electric push rod 26 is fixedly connected to the rear surface of the connecting plate 16.

[0025] The upper surface of the connecting plate 16 is fixedly connected with a housing 15 for providing physical protection for the monitoring device body 25. The upper surface of the housing 15 is fixedly connected with a cover 2, and the motor 1 is located inside the cover 2. The inner surface of the housing 15 is rotatably connected with a brush 24 for cleaning the panel of the monitoring device body 25. The brush 24 is movably connected to the monitoring device body 25. The upper surface of the housing 15 is fixedly connected with a motor 1, and the brush 24 is driven by the motor 1. The inner surface of the housing 15 is fixedly connected with a nozzle 23 for blowing away the dust and debris brushed off by the brush 24. The upper surface of the housing 15 is fixedly connected with an air pump 14, and the output end of the air pump 14 is communicated with a connecting pipe 13. The side surface of the connecting pipe 13 is communicated with the nozzle 23.

[0026] Working principle: When in use, place the device in a suitable position and fix the bottom plate 22 in place by the ground nails 11, so as to be fixed in place for a long time to stably monitor the orbit and status of the satellite. Drive the hydraulic rod 18 through the hydraulic cylinder 19 to drive the support column 17 to lift, so as to adjust the optimal height. Then, the monitoring device body 25 can be used to continuously monitor the satellites in space. When the device is on standby, drive the first slide bar 3 to retract through the electric push rod 26, so as to drive the housing 15 to move above the monitoring device body 25 to provide physical protection for the device, which can reduce the direct impact of external object impacts on the monitoring device body 25 and improve the anti-collision ability. Drive the brush 24 through the motor 1 to clean the dust on the surface of the monitoring device body 25, and blow away the dust through the nozzle 23, so as to achieve the self-cleaning function of the device, keep the equipment clean, and reduce the detection error.

[0027] The embodiments of the present utility model have been described in detail above in conjunction with the accompanying drawings. However, the present utility model is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present utility model within the scope of knowledge possessed by those of ordinary skill in the relevant art.

Claims

1. An intelligent monitoring device for accurate orbital flight of a microsatellite, characterized in that, Including: A bottom plate (22), the upper surface of the bottom plate (22) is fixedly connected with a bottom column (21), the upper end of the bottom column (21) is provided with a lifting assembly, the upper end of the lifting assembly is fixedly connected with a support column (17), the upper end of the support column (17) is fixedly connected with a bearing plate (4), the upper surface of the bearing plate (4) is fixedly connected with a monitoring device body (25), a through hole (27) is arranged on the bearing plate (4), the inner surface of the through hole (27) is slidably connected with a first slide rod (3), the other end of the first slide rod (3) is fixedly connected with a connecting plate (16), an installation hole is arranged on the bearing plate (4), the inner surface of the installation hole is fixedly connected with an electric push rod (26), and the other end of the electric push rod (26) is fixedly connected to the rear surface of the connecting plate (16); The upper surface of the connecting plate (16) is fixedly connected with a protective shell (15), the inner surface of the protective shell (15) is rotatably connected with a brush (24), the brush (24) is movably connected with the monitoring device body (25), the upper surface of the protective shell (15) is fixedly connected with a motor (1), the brush (24) is driven by the motor (1), the inner surface of the protective shell (15) is fixedly connected with a spray head (23), the upper surface of the protective shell (15) is fixedly connected with an air pump (14), the output end of the air pump (14) is communicated with a connecting pipe (13), and the side surface of the connecting pipe (13) is communicated with the spray head (23).

2. The intelligent monitoring device for precise orbital flight of a microsatellite according to claim 1, characterized in that, The lifting assembly includes: a hydraulic cylinder (19) and a hydraulic rod (18), the hydraulic cylinder (19) is fixedly connected to the upper end of the bottom column (21), the hydraulic rod (18) is fixedly connected to the output end of the hydraulic cylinder (19), and the support column (17) is fixedly connected to the upper end of the hydraulic rod (18).

3. An intelligent monitoring device for precise orbital flight of a microsatellite according to claim 1, characterized in that, The side surface of the bottom column (21) is fixedly connected with a lower fixing plate (20), and the upper surface of the lower fixing plate (20) is fixedly connected with a sleeve (8).

4. The intelligent monitoring device for precise orbital flight of a microsatellite according to claim 3, characterized in that, The side surface of the support column (17) is fixedly connected with an upper fixing plate (7), the lower surface of the upper fixing plate (7) is fixedly connected with a second slide rod (9), and the second slide rod (9) penetrates to the lower surface of the sleeve (8).

5. The intelligent monitoring device for precise orbital flight of a microsatellite according to claim 4, characterized in that, The lower end of the second slide rod (9) is fixedly connected with a limiting plate (10), and the limiting plate (10) is slidably connected with the lower fixing plate (20).

6. The intelligent monitoring device for precise orbital flight of a microsatellite according to claim 1, characterized in that, The side surface of the support column (17) is fixedly connected with a side plate (6), and the side surface of the side plate (6) is fixedly connected with a warning lamp (5).

7. The intelligent monitoring device for precise orbital flight of a microsatellite according to claim 1, characterized in that, A fixing hole (12) is fixedly connected to the bottom plate (22), and a ground nail (11) is movably connected inside the fixing hole (12).

8. An intelligent monitoring device for precise orbital flight of a microsatellite according to claim 1, characterized in that The upper surface of the protective shell (15) is fixedly connected with a cover shell (2), and the motor (1) is located inside the cover shell (2).

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