CN203250853U - Three-axis stabilization mobile tracking mount of shipborne satellite antenna - Google Patents
Three-axis stabilization mobile tracking mount of shipborne satellite antenna Download PDFInfo
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- CN203250853U CN203250853U CN 201320116336 CN201320116336U CN203250853U CN 203250853 U CN203250853 U CN 203250853U CN 201320116336 CN201320116336 CN 201320116336 CN 201320116336 U CN201320116336 U CN 201320116336U CN 203250853 U CN203250853 U CN 203250853U
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Abstract
The utility model provides a three-axis stabilization mobile tracking mount of a shipborne satellite antenna. The three-axis stabilization mobile tracking mount of the shipborne satellite antenna comprises a paraboloid antenna (1), a roll rotating shaft (2), a pitching rotating shaft (3), an orientation rotating shaft (4), a support (5) and a pedestal (6). According to the utility model, the above components form a three-axis rotating device, the orientation rotating shaft is fixedly connected in the bottom center of the pedestal upwards vertically, and the center of a crossbeam of the support is in rotation connection at the upper end of the orientation rotating shaft; the pitching rotating shaft can be arranged at the upper parts of the two upright racks of the support rotatably and horizontally, the roll rotating shaft is located above the center of the pitching rotating shaft to be in orthogonal connection with the pitching rotating shaft rotatably, and the paraboloid antenna is fixedly connected on the roll rotating shaft. By employing the technical scheme of using a feedback system which is composed of an photoelectric sensor, a position potentiometer, an angular velocity sensor, an electronic compass, a rotary encoder and a GPS receiver, to substitute a gyro system, the shipborne satellite antenna achieves the purposes of simplifying structure, reducing cost and facilitating civilianization.
Description
Technical field
The utility model relates to a kind of mobile tracking mount of Bearer Control satellite antenna, specifically refer to for carrying and control the Shipborne satellite antenna that is arranged on the boats and ships, along with the course variation of boats and ships and the fluctuating of waving of hull are jolted, the automatic track aiming geostatic telecommunications satellite is accepted the three-axis stabilization mobile tracking mount of a kind of Shipborne satellite antenna of satellite information.
Background technology
Be different from the ground satellite antenna, Shipborne satellite antenna is when tracking aiming target geostatic telecommunications satellite, except needs overcome the interference of strong wind air-flow, also need to change and the fluctuating of hull is waved and jolted along with the course of boats and ships, automatically control paraboloid satellite antenna run-home communications satellite carries out roll, pitching, azimuth rotation with motion tracking, prior art adopts and at the triple axle antenna pedestal inertia gyroscope to be set and surely to control paraboloid satellite antenna alignment target satellite to system and carry out servo-actuated pursuit movement, such as Chinese patent " Three-axis gyrostabilizer for shipborne antenna " 92231278.8; Because the gyro system complex structure, with high costs, be unfavorable for the commercial market application, therefore, prior art exist complex structure, with high costs, be difficult to civilian problems and shortcomings.
Summary of the invention
Problems and shortcomings for above-mentioned prior art existence, the utility model adopts by the roll rotating shaft, the pitching rotating shaft, direction rotating shaft, support, the triaxial rotating device of the carrying parabolic antenna that pedestal consists of, direction rotating shaft is fixedly connected on the center of base bottom vertically upward, the center rotating of the crossbeam of support is connected to the upper end of direction rotating shaft, the pitching rotating shaft rotatably is horizontally set on the top of two stands of support, the top that the roll rotating shaft is positioned at pitching spindle central position is connected with the rotatable quadrature of pitching rotating shaft, parabolic antenna be fixedly connected on the roll rotating shaft above; The bottom surface of pedestal is fixedly connected on the top of using boats and ships during application; Be used for control and drive the G servomotor that the roll rotation is done in the roll rotating shaft, and be connected all G feedback units of the monitoring roll rotating shaft attitude that G photoelectric sensor, G position potentiometer, G angular-rate sensor consist of and be arranged on pitching rotating shaft place and be connected with computer controller; Be used for control and drive the Y servomotor that the pitching rotation is done in the pitching rotating shaft, be connected all Y feedback units of the monitoring pitching rotating shaft attitude that Y photoelectric sensor, Y position potentiometer, Y angular-rate sensor, Y electronic compass consist of be arranged on support stand the place, top and be connected with computer controller; Be used for the control driving arm and make the F servomotor of orientation rotation at direction rotating shaft, be arranged on the crossbeam place of support with all F feedback units in the monitoring direction rotating shaft orientation that is consisted of by F angular-rate sensor, F electronic compass, rotary encoder, be used for also being arranged on the crossbeam place of support with GPS receiver that the GPS position location satellite carries out Geographic mapping and being connected with computer controller;
During application, the signal of the feedback of all feedback units and GPS is processed with the beam tracking mode by computer controller, control each axle servomotor and drive respectively the roll rotating shaft, the pitching rotating shaft, the direction rotating shaft rotation, driving parabolic antenna waves the run-home communications satellite that jolts and carries out closed loop with the technical scheme of motion tracking along with the fluctuating of hull, a kind of three-axis stabilization mobile tracking mount of Shipborne satellite antenna is provided, the reponse system that is intended to utilize all feedback units to consist of comes alternative structure complicated, gyro system with high costs makes Shipborne satellite antenna reach simplified structure to reduce cost, reduce cost, be easy to the purpose of civil nature.
The purpose of this utility model is achieved in that a kind of three-axis stabilization mobile tracking mount of Shipborne satellite antenna, comprise parabolic antenna, roll rotating shaft, pitching rotating shaft, direction rotating shaft, support, pedestal, wherein: described parabolic antenna is the thin-wall aluminum alloy matter member of paraboloidal; The focus place of parabolic antenna is provided with satellite-signal and accepts head;
Described roll rotating shaft is made the rotating shaft mechanism that roll is rotated for the carrying parabolic antenna in the pitching rotating shaft;
The rotating shaft mechanism of pitch rotation is made in described pitching rotating shaft at support for carrying roll rotating shaft;
Described direction rotating shaft is bearing support is made azimuth rotation at pedestal rotating shaft mechanism;
Described support is for to be made of crossbeam, stand, and the steel components of rectangular inverted doorframe shape, described cross beam water prosposition be in the bottom of support, two stand symmetries straight up be positioned at crossbeam about two ends;
Described pedestal is that opened upper end, bottom have the end to be the steel thin wall member of drum-shaped;
Direction rotating shaft is fixedly connected on the center of base bottom vertically upward, the center rotating of the described crossbeam of support is connected to the upper end of direction rotating shaft, the pitching rotating shaft rotatably is horizontally set on the top of two described stands of support, the top that the roll rotating shaft is positioned at pitching spindle central position is connected with the rotatable quadrature of pitching rotating shaft, parabolic antenna be fixedly connected on the roll rotating shaft above; The bottom surface of pedestal is fixedly connected on the top of using boats and ships during application;
Be used for control and drive the G servomotor that the roll rotation is done in the roll rotating shaft, be arranged on pitching rotating shaft place with all G feedback units of the monitoring roll rotating shaft attitude that is consisted of by G photoelectric sensor, G position potentiometer, G angular-rate sensor, and be connected with computer controller by wire or feeder line respectively; Be used for control and drive the Y servomotor that the pitching rotation is done in the pitching rotating shaft, be arranged on the place, top of the stand of support with all Y feedback units of the monitoring pitching rotating shaft attitude that is consisted of by Y photoelectric sensor, Y position potentiometer, Y angular-rate sensor, Y electronic compass, and be connected with computer controller by wire or feeder line respectively; Be used for the control driving arm and make the F servomotor of orientation rotation at direction rotating shaft, be arranged on the crossbeam place of support with all F feedback units in the monitoring direction rotating shaft orientation that is consisted of by F angular-rate sensor, F electronic compass, rotary encoder, the GPS receiver that is used for carrying out with the GPS position location satellite Geographic mapping also is arranged on the crossbeam place of support, and is connected with computer controller by wire or feeder line respectively;
Described photoelectric sensor is to utilize object to be detected to shading or the reflection of Infrared, comes the electronic installation that has or not of inspected object by gating and cut-off; Described position potentiometer is measured the electronic installation of the spin angular position of tested rotation axis for changing output voltage by the gear driven adjustable resistance; Described angular-rate sensor is for being used for measuring the inertia angular speed piezoelectric transducer of tested rotation axis angular velocity of rotation; Described electronic compass is the folded azimuth of the north and south pole axis that is used for the given horizontal direction axis of its carrier of living in of mensuration and the earth, and for the electronic installation of measuring the folded inclination angle of the given vertical axis of its carrier of living in and terrestrial gravitation vertical line; Described GPS receiver be by with the communication of GPS position location satellite, the geographical coordinate of its carrier of living in is carried out the receiving system of longitude, latitude and height Accurate Measurement above sea level; Described computer controller is for obtaining target satellite beam maximum gain with acceptance, by the data of described G feedback unit, Y feedback unit, F feedback unit and GPS receiver feedback are processed, control respectively G servomotor, Y servomotor, F driven by servomotor roll rotating shaft, pitching rotating shaft, direction rotating shaft rotation, drive the computer control device that is provided with display terminal of parabolic antenna tracking target satellite;
Described roll is rotated, and is establishing straight line with the plane of sea level quadrature, this straight line by on this straight line a bit centered by do rotation with the sea level keeping parallelism; Described pitch rotation is, if one with the vertical line of sea level quadrature, centered by the joining on vertical line and sea level, cross described center and establish one at the ray above the sea level and between the vertical line, ray is done in the rotation above the sea level and between the vertical line take described center as pivot; Described azimuth rotation is, establishes a straight line with terrestrial gravitation vertical line quadrature, this straight line by with the joining of terrestrial gravitation vertical line centered by do rotation around the terrestrial gravitation vertical line.
Operation principle and beneficial effect
During application, along with the fluctuating of hull is waved and is jolted, computer controller is processed the signal of the feedback of described all G, all Y, all F feedback units with the beam tracking mode, control described G servomotor, Y servomotor, F servomotor and drive respectively roll rotating shaft, pitching rotating shaft, direction rotating shaft rotation, drive parabolic antenna run-home communications satellite and carry out closed loop with motion tracking; Wherein, the roll rotating shaft is for correcting the folded inclination angle in parabolic antenna and sea level along with the oscillating motion of boats and ships, and the horizontal line that keeps parabolic antenna to set is servo-actuated parallel with the sea level; The pitching rotating shaft is used for along with the aim at the mark angle of pitch of communications satellite of parabolic antenna is corrected in the undulatory motion of boats and ships; Direction rotating shaft is for correct the folded azimuthal change of parabolic antenna and earth south poles along with the navigation direction variation of boats and ships.
The reponse system that this device utilizes described all feedback units to consist of comes complicated, the with high costs gyro system of alternative structure to reduce cost, make Shipborne satellite antenna simplify the structure, reduce cost, be conducive to the application of the ships for civil use such as fishing boat, pleasure-boat, yacht.
Above-mentioned, the utility model adopts the triaxial rotating device of the carrying parabolic antenna that is made of roll rotating shaft, pitching rotating shaft, direction rotating shaft, support, pedestal, direction rotating shaft is fixedly connected on the center of base bottom vertically upward, the center rotating of the described crossbeam of support is connected to the upper end of direction rotating shaft, the pitching rotating shaft rotatably is horizontally set on the top of two described stands of support, the top that the roll rotating shaft is positioned at pitching spindle central position is connected with the rotatable quadrature of pitching rotating shaft, parabolic antenna be fixedly connected on the roll rotating shaft above; The bottom surface of pedestal is fixedly connected on the top of using boats and ships during application; And be provided with for respectively control driving roll rotating shaft, the pitching rotating shaft, the servomotor of direction rotating shaft three axle work, be used for the described three axle operating attitudes of respectively monitoring feedback by photoelectric sensor, the position potentiometer, angular-rate sensor, electronic compass, the technical scheme of all feedback units that the GPS receiver consists of, the three-axis stabilization mobile tracking mount of a kind of Shipborne satellite antenna that provides, the reponse system of utilizing all feedback units to consist of comes alternative structure complicated, gyro system with high costs makes Shipborne satellite antenna reach simplified structure to reduce cost, reduce cost, be easy to the purpose of civil nature.
Description of drawings
Fig. 1 is the structural representation of the three-axis stabilization mobile tracking mount of a kind of Shipborne satellite antenna of the present utility model.
Below in conjunction with the embodiment in the accompanying drawing the utility model is described in further detail, but should not be construed as any restriction of the present utility model.
Among the figure: parabolic antenna 1, roll rotating shaft 2, G servomotor 21, G photoelectric sensor 22, G position potentiometer 23, G angular-rate sensor 24, pitching rotating shaft 3, Y servomotor 31, Y photoelectric sensor 32, Y position potentiometer 33, Y angular-rate sensor 34, Y electronic compass 35, direction rotating shaft 4, F servomotor 41, F angular-rate sensor 42, F electronic compass 43, rotary encoder 44, GPS receiver 45, support 5, crossbeam 51, stand 52, pedestal 6, Timing Belt 01.
Embodiment
Consult Fig. 1, the three-axis stabilization mobile tracking mount of a kind of Shipborne satellite antenna of the present utility model, comprise parabolic antenna 1, roll rotating shaft 2, pitching rotating shaft 3, direction rotating shaft 4, support 5, pedestal 6, wherein: the thin-wall aluminum alloy matter member that described parabolic antenna 1 is paraboloidal; The focus place of parabolic antenna 1 is provided with satellite-signal and accepts head;
Described roll rotating shaft 2 is made the rotating shaft mechanism that roll is rotated for carrying parabolic antenna 1 in pitching rotating shaft 3;
The rotating shaft mechanism of pitch rotation is made in described pitching rotating shaft 3 at support 5 for carrying roll rotating shaft 2;
Described direction rotating shaft 4 is made the rotating shaft mechanism of azimuth rotation at pedestal 6 for bearing support 5;
Described support 5 is for to be made of crossbeam 51, stand 52, the steel components of rectangular inverted doorframe shape, described crossbeam 51 levels are positioned at the bottom of support 5, two stand 52 symmetries straight up be positioned at crossbeam 51 about two ends;
Described pedestal 6 has the end to be the steel thin wall member of drum-shaped for opened upper end, bottom;
Be used for control and drive the G servomotor 21 that the roll rotation is done in roll rotating shaft 2, be arranged on pitching rotating shaft 3 places with all G feedback units of monitoring roll rotating shaft 2 attitudes that consisted of by G photoelectric sensor 22, G position potentiometer 23, G angular-rate sensor 24, and be connected with computer controller by wire or feeder line respectively; Be used for control and drive the Y servomotor 31 that the pitching rotation is done in pitching rotating shaft 3, be arranged on the place, top of the stand 52 of support 5 with all Y feedback units of monitoring pitching rotating shaft 3 attitudes that consisted of by Y photoelectric sensor 32, Y position potentiometer 33, Y angular-rate sensor 34, Y electronic compass 35, and be connected with computer controller by wire or feeder line respectively; Be used for control driving arm 5 and make the F servomotor 41 of orientation rotation at direction rotating shaft 4, be arranged on crossbeam 51 places of support 5 with all F feedback units in monitoring direction rotating shaft 4 orientation that consisted of by F angular-rate sensor 42, F electronic compass 43, rotary encoder 44, the GPS receiver 45 that is used for carrying out with the GPS position location satellite Geographic mapping also is arranged on crossbeam 51 places of support 5, and is connected with computer controller by wire or feeder line respectively;
Described photoelectric sensor is to utilize object to be detected to shading or the reflection of Infrared, comes the electronic installation that has or not of inspected object by gating and cut-off; Described position potentiometer is measured the electronic installation of the spin angular position of tested rotation axis for changing output voltage by the gear driven adjustable resistance; Described angular-rate sensor is for being used for measuring the inertia angular speed piezoelectric transducer of tested rotation axis angular velocity of rotation; Described electronic compass is the folded azimuth of the north and south pole axis that is used for the given horizontal direction axis of its carrier of living in of mensuration and the earth, and for the electronic installation of measuring the folded inclination angle of the given vertical axis of its carrier of living in and terrestrial gravitation vertical line; Described GPS receiver 45 be by with the communication of GPS position location satellite, the geographical coordinate of its carrier of living in is carried out the receiving system of longitude, latitude and height Accurate Measurement above sea level; Described computer controller is for obtaining target satellite beam maximum gain with acceptance, by the data of described G feedback unit, Y feedback unit, F feedback unit and GPS receiver 45 feedbacks are processed, control respectively G servomotor 21, Y servomotor 31, the 41 driving roll rotating shafts 2 of F servomotor, pitching rotating shaft 3, direction rotating shaft 4 rotations, drive the computer control device that is provided with display terminal of parabolic antenna 1 tracking target satellite;
Described roll is rotated, and is establishing straight line with the plane of sea level quadrature, this straight line by on this straight line a bit centered by do rotation with the sea level keeping parallelism; Described pitch rotation is, if one with the vertical line of sea level quadrature, centered by the joining on vertical line and sea level, cross described center and establish one at the ray above the sea level and between the vertical line, ray is done in the rotation above the sea level and between the vertical line take described center as pivot; Described azimuth rotation is, establishes a straight line with terrestrial gravitation vertical line quadrature, this straight line by with the joining of terrestrial gravitation vertical line centered by do rotation around the terrestrial gravitation vertical line.
Operation principle and beneficial effect
During application, along with the fluctuating of hull is waved and is jolted, computer controller is processed the signal of the feedback of described all G, all Y, all F feedback units with the beam tracking mode, control described G servomotor 21, Y servomotor 31, F servomotor 41 and drive respectively roll rotating shaft 2, pitching rotating shaft 3, direction rotating shaft 4 rotations, drive parabolic antenna 1 run-home communications satellite and carry out closed loop with motion tracking; Wherein, roll rotating shaft 2 is for correcting the folded inclination angle in parabolic antenna 1 and sea level along with the oscillating motion of boats and ships, and the horizontal line that keeps parabolic antenna 1 to set is servo-actuated parallel with the sea level; Pitching rotating shaft 3 is used for along with the aim at the mark angle of pitch of communications satellite of parabolic antenna 1 is corrected in the undulatory motion of boats and ships; Direction rotating shaft 4 is for correct the folded azimuthal change of parabolic antenna 1 and earth south poles along with the navigation direction variation of boats and ships.
The reponse system that this device utilizes described all feedback units to consist of comes complicated, the with high costs gyro system of alternative structure to reduce cost, make Shipborne satellite antenna simplify the structure, reduce cost, be conducive to the application of the ships for civil use such as fishing boat, pleasure-boat, yacht.
Claims (1)
1. the three-axis stabilization mobile tracking mount of a Shipborne satellite antenna, comprise parabolic antenna (1), roll rotating shaft (2), pitching rotating shaft (3), direction rotating shaft (4), support (5), pedestal (6), it is characterized in that: described parabolic antenna (1) is the thin-wall aluminum alloy matter member of paraboloidal; The focus place of parabolic antenna (1) is provided with satellite-signal and accepts head;
Described roll rotating shaft (2) is made the rotating shaft mechanism that roll is rotated for carrying parabolic antenna (1) in pitching rotating shaft (3);
The rotating shaft mechanism of pitch rotation is made in described pitching rotating shaft (3) at support (5) for carrying roll rotating shaft (2);
Described direction rotating shaft (4) is made the rotating shaft mechanism of azimuth rotation at pedestal (6) for bearing support (5);
Described support (5) is to be made of crossbeam (51), stand (52), the steel components of rectangular inverted doorframe shape, described crossbeam (51) level is positioned at the bottom of support (5), two stand (52) symmetries straight up be positioned at crossbeam (51) about two ends;
Described pedestal (6) is that opened upper end, bottom have the end to be the steel thin wall member of drum-shaped;
Direction rotating shaft (4) is fixedly connected on the center of pedestal (6) bottom vertically upward, the center rotating of the described crossbeam (51) of support (5) is connected to the upper end of direction rotating shaft (4), pitching rotating shaft (3) rotatably is horizontally set on the top of two described stands (52) of support (5), the top that roll rotating shaft (2) is positioned at pitching rotating shaft (3) center is connected with the rotatable quadrature of pitching rotating shaft (3), parabolic antenna (1) be fixedly connected on roll rotating shaft (2) above; The bottom surface of pedestal during application (6) is fixedly connected on the top of using boats and ships;
Be used for control and drive the G servomotor (21) that the roll rotation is done in roll rotating shaft (2), be arranged on pitching rotating shaft (3) with all G feedback units of monitoring roll rotating shaft (2) attitude that is consisted of by G photoelectric sensor (22), G position potentiometer (23), G angular-rate sensor (24) and locate, and be connected with computer controller by wire or feeder line respectively; Be used for control and drive the Y servomotor (31) that the pitching rotation is done in pitching rotating shaft (3), be arranged on the place, top of the stand (52) of support (5) with all Y feedback units of monitoring pitching rotating shaft (3) attitude that is consisted of by Y photoelectric sensor (32), Y position potentiometer (33), Y angular-rate sensor (34), Y electronic compass (35), and be connected with computer controller by wire or feeder line respectively; Be used for control driving arm (5) and make the F servomotor (41) of orientation rotation at direction rotating shaft (4), with by F angular-rate sensor (42), F electronic compass (43), all F feedback units in monitoring direction rotating shaft (4) orientation that rotary encoder (44) consists of are arranged on the crossbeam (51) of support (5) and locate, the GPS receiver (45) that is used for carrying out Geographic mapping with the GPS position location satellite also is arranged on the crossbeam (51) of support (5) and locates, and is connected with computer controller by wire or feeder line respectively;
Described photoelectric sensor is to utilize object to be detected to shading or the reflection of Infrared, comes the electronic installation that has or not of inspected object by gating and cut-off; Described position potentiometer is measured the electronic installation of the spin angular position of tested rotation axis for changing output voltage by the gear driven adjustable resistance; Described angular-rate sensor is for being used for measuring the inertia angular speed piezoelectric transducer of tested rotation axis angular velocity of rotation; Described electronic compass is the folded azimuth of the north and south pole axis that is used for the given horizontal direction axis of its carrier of living in of mensuration and the earth, and for the electronic installation of measuring the folded inclination angle of the given vertical axis of its carrier of living in and terrestrial gravitation vertical line; Described GPS receiver (45) be by with the communication of GPS position location satellite, the geographical coordinate of its carrier of living in is carried out the receiving system of longitude, latitude and height Accurate Measurement above sea level; Described computer controller is for obtaining target satellite beam maximum gain with acceptance, by the data of described G feedback unit, Y feedback unit, F feedback unit and GPS receiver (45) feedback are processed, control respectively G servomotor (21), Y servomotor (31), F servomotor (41) driving roll rotating shaft (2), pitching rotating shaft (3), direction rotating shaft (4) rotation, drive the computer control device that is provided with display terminal of parabolic antenna (1) tracking target satellite;
Described roll is rotated, and is establishing straight line with the plane of sea level quadrature, this straight line by on this straight line a bit centered by do rotation with the sea level keeping parallelism; Described pitch rotation is, if one with the vertical line of sea level quadrature, centered by the joining on vertical line and sea level, cross described center and establish one at the ray above the sea level and between the vertical line, ray is done in the rotation above the sea level and between the vertical line take described center as pivot; Described azimuth rotation is, establishes a straight line with terrestrial gravitation vertical line quadrature, this straight line by with the joining of terrestrial gravitation vertical line centered by do rotation around the terrestrial gravitation vertical line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320116336 CN203250853U (en) | 2013-02-27 | 2013-02-27 | Three-axis stabilization mobile tracking mount of shipborne satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320116336 CN203250853U (en) | 2013-02-27 | 2013-02-27 | Three-axis stabilization mobile tracking mount of shipborne satellite antenna |
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| Publication Number | Publication Date |
|---|---|
| CN203250853U true CN203250853U (en) | 2013-10-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320116336 Withdrawn - After Issue CN203250853U (en) | 2013-02-27 | 2013-02-27 | Three-axis stabilization mobile tracking mount of shipborne satellite antenna |
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| CN (1) | CN203250853U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103138050A (en) * | 2013-02-27 | 2013-06-05 | 宁波森富机电制造有限公司 | Three-axis stable follow-up tracking device of shipborne satellite antenna |
| CN104990458A (en) * | 2015-06-29 | 2015-10-21 | 南京理工大学 | Pull rod type infrared imaging seeker position marker |
| CN104990457A (en) * | 2015-06-29 | 2015-10-21 | 南京理工大学 | Direct drive type infrared imaging seeker position marker |
| CN105281017A (en) * | 2014-07-09 | 2016-01-27 | 北京星网卫通科技开发有限公司 | Shipborne satellite communication antenna |
| CN105281015A (en) * | 2015-05-08 | 2016-01-27 | 北京中星讯达科技有限公司 | Two-dimension follow-up communication-in-moving satellite communication antenna structure |
| CN106814754A (en) * | 2017-03-28 | 2017-06-09 | 东莞松山湖国际机器人研究院有限公司 | A kind of three axle heads, shooting robot and control method |
| CN107505953A (en) * | 2017-10-13 | 2017-12-22 | 南昌大学 | A kind of unmanned plane automatic tracking antenna system and its tracking |
| CN109216922A (en) * | 2018-10-26 | 2019-01-15 | 浙江中星光电子科技有限公司 | A kind of satellite antenna pitching angle homeostasis regulating device |
| CN109786967A (en) * | 2019-03-04 | 2019-05-21 | 大连理工大学 | A kind of ship-board antenna attitude control system of high-precision real-time tracking |
| CN115185304A (en) * | 2022-07-08 | 2022-10-14 | 天津飞图科技有限公司 | Novel satellite tracking rotating platform |
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2013
- 2013-02-27 CN CN 201320116336 patent/CN203250853U/en not_active Withdrawn - After Issue
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103138050B (en) * | 2013-02-27 | 2015-01-14 | 宁波森富机电制造有限公司 | Three-axis stable follow-up tracking device of shipborne satellite antenna |
| CN103138050A (en) * | 2013-02-27 | 2013-06-05 | 宁波森富机电制造有限公司 | Three-axis stable follow-up tracking device of shipborne satellite antenna |
| CN105281017B (en) * | 2014-07-09 | 2018-01-02 | 北京星网卫通科技开发有限公司 | A kind of boat-carrying satellite communication antena |
| CN105281017A (en) * | 2014-07-09 | 2016-01-27 | 北京星网卫通科技开发有限公司 | Shipborne satellite communication antenna |
| CN105281015B (en) * | 2015-05-08 | 2018-06-05 | 北京中星讯达科技有限公司 | A kind of servo-actuated communication in moving satellite communication antenna structure of two dimension |
| CN105281015A (en) * | 2015-05-08 | 2016-01-27 | 北京中星讯达科技有限公司 | Two-dimension follow-up communication-in-moving satellite communication antenna structure |
| CN104990457A (en) * | 2015-06-29 | 2015-10-21 | 南京理工大学 | Direct drive type infrared imaging seeker position marker |
| CN104990458A (en) * | 2015-06-29 | 2015-10-21 | 南京理工大学 | Pull rod type infrared imaging seeker position marker |
| CN106814754A (en) * | 2017-03-28 | 2017-06-09 | 东莞松山湖国际机器人研究院有限公司 | A kind of three axle heads, shooting robot and control method |
| CN107505953A (en) * | 2017-10-13 | 2017-12-22 | 南昌大学 | A kind of unmanned plane automatic tracking antenna system and its tracking |
| CN107505953B (en) * | 2017-10-13 | 2024-02-20 | 南昌大学 | Unmanned aerial vehicle automatic tracking antenna system and tracking method thereof |
| CN109216922A (en) * | 2018-10-26 | 2019-01-15 | 浙江中星光电子科技有限公司 | A kind of satellite antenna pitching angle homeostasis regulating device |
| CN109786967A (en) * | 2019-03-04 | 2019-05-21 | 大连理工大学 | A kind of ship-board antenna attitude control system of high-precision real-time tracking |
| CN115185304A (en) * | 2022-07-08 | 2022-10-14 | 天津飞图科技有限公司 | Novel satellite tracking rotating platform |
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