CN205069857U - Gamut directional antenna system - Google Patents
Gamut directional antenna system Download PDFInfo
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- CN205069857U CN205069857U CN201520729508.5U CN201520729508U CN205069857U CN 205069857 U CN205069857 U CN 205069857U CN 201520729508 U CN201520729508 U CN 201520729508U CN 205069857 U CN205069857 U CN 205069857U
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Abstract
The utility model belongs to the technical field of communication equipment, especially, relate to a gamut directional antenna system. It has solved the little scheduling problem of current directional aerial coverage area. Including ground satellite station's support body and airborne vehicle, its characterized in that, ground satellite station's support body on have at least one activity direction ground directional aerial, the airborne vehicle on have that at least one activity direction is put and can carry out bi -directional data transmission's aviation directional aerial with ground directional aerial, thereby aviation directional aerial and ground directional aerial between be equipped with the power antenan device that enables aviation directional aerial and/or ground directional aerial free rotation and make aviation directional aerial orientation and ground directional aerial orientation correspond each other all the time. This gamut directional antenna system's advantage lies in: simple structure, stability is good, and the coverage is big, can realize that receiving antenna and emit antenna correspond all the time each other, can realize that the full angle of antenna covers, and the communication is of high quality.
Description
Technical field
The utility model belongs to technical field of communication equipment, especially relates to a kind of gamut beam aerial system.
Background technology
In wireless telecommunication system, according to the difference of directivity, antenna system is divided into omnidirectional antenna and directional antenna two kinds, omnidirectional antenna can in the horizontal direction 360 degree all homogeneous radiations, coverage is large, but omnidirectional antenna is when equal transmitting power, and the signal distance emitter that receiver receives is nearer, applications distances is short, can only be applicable to short-range Signal transmissions scene.Directional antenna refers to be launched and to receive electromagnetic wave strong especially on some or certain several direction, and launching in the other direction and receiving electromagnetic wave is then zero or minimum a kind of antenna.Adopt the object of directional transmitting antenna to be the effective rate of utilization increasing radiant power, increase confidentiality; The object of directional receiving antenna is adopted to be strengthen signal strength signal intensity to increase antijamming capability.Directional antenna has: larger forward gain; Can backward signal be suppressed, avoid backward interference; Under the prerequisite of equal emitter power, the advantages such as the scope of the receiver Received signal strength on assigned direction can be increased, but directional antenna is owing to can only carry out the transmission of signal in given directions, and effective Signal transmissions cannot be carried out in other directions, directional antenna is so just made to exist: coverage is less, full angle covering cannot be carried out, the problems such as communication quality difference.Therefore, how the feature of omnidirectional antenna and directional antenna to be combined thus the flexibility improving directional antenna is a technical problem being badly in need of solving.
In order to solve prior art Problems existing, people have carried out long-term exploration, propose solution miscellaneous.Such as, Chinese patent literature discloses a kind of automatic direction-finding aerial system, the automatic orientation method of antenna and device [application number: 201210591627.X], comprise: the first stepping motor be connected with horizontal drive mechanism and the vertical transmission mechanism of antenna respectively and the second stepping motor and electronic compass, by the first stepping motor and the second stepping motor, antenna can be rotated in horizontal dimensions and vertical dimensions, by obtaining the current azimuth of antenna and the angle of pitch, and the geographical location information of antenna and destination node carries out adjustment control to the sensing of antenna, make when antenna and destination node exist larger difference in height, also by the sensing in the vertical direction of adjustment antenna, improve the communication quality of antenna and signal projector.
Such scheme to some extent solves the problem of existing directional antenna very flexible, but the program still also exists: reception antenna cannot be realized mutually corresponding all the time with transmitting antenna, the problems such as coverage is less, cannot carry out full angle covering, communication quality difference.
Summary of the invention
The purpose of this utility model is for the problems referred to above, provides a kind of simple and reasonable, the gamut beam aerial system that reception antenna and transmitting antenna full angle cover.
For achieving the above object, the utility model have employed following technical proposal: this gamut beam aerial system, comprise ground station's support body and airborne vehicle, it is characterized in that, described ground station's support body has the surface orientation antenna of at least one activity direction, described airborne vehicle has at least one activity direction put and the directional aviation antenna of bidirectional data transfers can be carried out with surface orientation antenna, described directional aviation antenna be provided with between surface orientation antenna directional aviation antenna and/or surface orientation antenna can be made freely to rotate thus make directional aviation antenna towards with surface orientation antenna towards ACU antenna control unit mutually corresponding all the time.Preferably, directional aviation antenna here and surface orientation antenna synchronous axial system, so no matter airborne vehicle is in any position, and directional aviation antenna and surface orientation antenna all can be mutually corresponding, thus the gamut realizing directional antenna covers.
In above-mentioned gamut beam aerial system, described ACU antenna control unit comprise to be arranged between ground station's support body and surface orientation antenna and can according to directional aviation aerial position adjust surface orientation antenna towards thus make the ground-plane antenna adjust structure of surface orientation antenna direction directional aviation antenna, be provided with between described airborne vehicle and directional aviation antenna can according to directional antenna position, ground adjust directional aviation antenna towards thus make the aerodiscone antenna adjust structure of directional aviation antenna direction surface orientation antenna.Make like this surface orientation antenna and directional aviation antenna can respectively according to the position of the other side adjust self towards thus make that surface orientation antenna and directional aviation antenna are mutually corresponding all the time to be arranged.
In above-mentioned gamut beam aerial system, described ground-plane antenna adjust structure comprises circumference and rotates the first housing being arranged on ground station's support body upper end, described surface orientation antenna is hinged is arranged on the first housing upper end, the activity direction that the rotation direction that the first described housing and ground station support body are rotatedly connected and the first housing and surface orientation antenna are hinged and connected is different, the first circumferential rotating drive mechanism that the first housing can be made to rotate relative to ground station's support body circumference is provided with between the first described housing and ground station's support body, first swing driving mechanism that surface orientation antenna can be made relative to the first housing circuit oscillation is provided with between the first described housing and surface orientation antenna, described first circumferential rotating drive mechanism and the first swing driving mechanism are connected with the MPU module be arranged in the first housing respectively, a described MPU module is connected with the first GPS module be arranged in the first housing, and a described MPU module is all connected with the first supply module be arranged in the first housing with the first GPS module, first housing is provided with the display module be connected with a MPU module.Namely the first GPS module is here used for determining directional antenna position, ground, one MPU module obtains the first GPS module information and sends to directional aviation antenna, here surface orientation antenna and directional aviation antenna are bidirectional data transfers, one MPU module makes the first circumferential rotating drive mechanism and the first swing driving mechanism adjust the angle of surface orientation antenna, makes it all the time towards directional aviation antenna.
In above-mentioned gamut beam aerial system, described first circumferential rotating drive mechanism comprises the support being arranged on ground station's support body upper end, the first rotational drive motor be connected with a MPU module is provided with between described support with the first housing, the first described rotational drive motor is arranged on support or the first housing, and the output shaft of the first described rotational drive motor and the first housing or support are fixedly linked; Described ground station's support body comprises at least three bodies of rod, and described body of rod one end crosses and is all connected with support, and the described body of rod other end is tilted to down respectively and circumference is uniformly distributed setting; The first described rotational drive motor is stepping motor or brushless electric machine.Namely the first rotational drive motor here drives surface orientation antenna circumference rotate thus realize the adjustment of surface orientation antenna circumferential position.
In above-mentioned gamut beam aerial system, the first described swing driving mechanism comprises the first installing rack rotating and be arranged on the first housing upper end, described surface orientation antenna is arranged on the first installing rack, and is provided with the first wobble component assembly that can drive the first installing rack circuit oscillation between the first described installing rack and the first housing.
In above-mentioned gamut beam aerial system, the first described wobble component assembly comprises two correspondences and to be arranged in the first housing and be all connected with a MPU module first to drive steering wheel, described first drives the output shaft of steering wheel to pass the first housing respectively, the first described installing rack two ends are bent to form the first installation portion towards the first hull outside respectively, and described the first installation part does not drive the output shaft of steering wheel to be connected with first; The first described installing rack is bending, and has outward extending location division in the middle part of the first described installing rack, and described surface orientation antenna is arranged on location division.Namely steering wheel is driven to adjust surface orientation antenna pendulum angle by first, the adjustment of combined ground directional antenna circumferential position thus realize the universal position adjustment of surface orientation antenna.
In above-mentioned gamut beam aerial system, described aerodiscone antenna adjust structure comprises circumference and rotates the second housing being arranged on airborne vehicle bottom side, the described hinged setting of directional aviation antenna on the second housing and described directional aviation antenna is tilted to lower setting on rear side of airborne vehicle body, be provided with between the second described housing and airborne vehicle and can make the second housing relative to the circumferential second week rotated of airborne vehicle to rotating drive mechanism, second swing driving mechanism that directional aviation antenna can be made to swing relative to the second housing is provided with between the second described housing and directional aviation antenna, described second week is connected with the 2nd MPU module be arranged in the second housing to rotating drive mechanism respectively with the second swing driving mechanism, the 2nd described MPU module with to be arranged in the second housing and to be connected with the second GPS module that the first GPS module matches, and the 2nd described MPU module is all connected with the second supply module be arranged in the second housing with the second GPS module.Namely the second GPS module is here used for determining directional aviation aerial position, 2nd MPU module obtains the second GPS module information and sends to surface orientation antenna, here surface orientation antenna and directional aviation antenna are bidirectional data transfers, 2nd MPU module makes second week adjust the angle of directional aviation antenna to rotating drive mechanism and the second swing driving mechanism, makes it all the time towards surface orientation antenna.
In above-mentioned gamut beam aerial system, described second week comprises the Connection Block be arranged in the middle part of airborne vehicle bottom side to rotating drive mechanism, the second rotational drive motor be connected with the 2nd MPU module is provided with between described Connection Block with the second housing, the second described rotational drive motor is arranged on Connection Block or the second housing, and the output shaft of the second described rotational drive motor and the second housing or Connection Block are fixedly linked; Described airborne vehicle is any one or multiple combination in unmanned plane, dirigible and balloon; The second described rotational drive motor is stepping motor or brushless electric machine.Namely the second rotational drive motor here drives directional aviation antenna circumference rotate thus realize the adjustment of directional aviation antenna circumferential position.
In above-mentioned gamut beam aerial system, the second described swing driving mechanism comprises and is hingedly arranged on the second housing upper end and sweeping second installing rack, described directional aviation antenna is arranged in the middle part of the second installing rack, and is provided with the second wobble drive assembly that can drive the second installing rack circuit oscillation between the second described installing rack and the second housing.
In above-mentioned gamut beam aerial system, the second described wobble drive assembly comprises two correspondences and to be arranged in the second housing and be all connected with the 2nd MPU module second to drive steering wheel, described second drives the output shaft of steering wheel to pass the second housing respectively, the second described installing rack two ends are bent to form the second installation portion towards the second hull outside respectively, and the second described installation portion drives the output shaft of steering wheel to be connected with second respectively.Namely drive steering wheel to adjust directional aviation antenna pendulum angle by second, in conjunction with directional aviation antenna circumferential position adjustment thus realize the adjustment of directional aviation antenna universal position.
Compared with prior art, the advantage of this gamut beam aerial system is: structure is simple, good stability, and coverage is large, can realize reception antenna mutually corresponding all the time with transmitting antenna, and can realize antenna full angle and cover, communication quality is good.
Accompanying drawing explanation
The overall system architecture schematic diagram that Fig. 1 provides for the utility model.
The system architecture diagram that Fig. 2 provides for the utility model.
The structural representation of the ground-plane antenna adjust structure that Fig. 3 provides for the utility model.
The partial structurtes schematic diagram of the ground-plane antenna adjust structure that Fig. 4 provides for the utility model.
The structural representation of the aerodiscone antenna adjust structure that Fig. 5 provides for the utility model.
The partial structurtes schematic diagram of the aerodiscone antenna adjust structure that Fig. 6 provides for the utility model.
The partial structurtes schematic diagram at another visual angle of the aerodiscone antenna adjust structure that Fig. 7 provides for the utility model.
The partial sectional view of the aerodiscone antenna adjust structure that Fig. 8 provides for the utility model.
In figure, ground station's support body 1, the body of rod 11, airborne vehicle 2, surface orientation antenna 3, directional aviation antenna 4, ground-plane antenna adjust structure 5, first housing 51, first circumferential rotating drive mechanism 52, support 521, first rotational drive motor 522, first swing driving mechanism 53, first installing rack 531, first drives steering wheel 532, first installation portion 533, location division 534, one MPU module 54, first GPS module 55, first supply module 56, display module 57, aerodiscone antenna adjust structure 6, second housing 61, second week is to rotating drive mechanism 62, Connection Block 621, second rotational drive motor 622, second swing driving mechanism 63, second installing rack 631, second drives steering wheel 632, second installation portion 633, 2nd MPU module 64, second GPS module 65, second supply module 66.
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is described in more detail.
As shown in Figure 1-2, this gamut beam aerial system, comprise ground station's support body 1 and airborne vehicle 2, ground station's support body 1 has the surface orientation antenna 3 of at least one activity direction, airborne vehicle 2 has at least one activity direction put and the directional aviation antenna 4 of bidirectional data transfers can be carried out with surface orientation antenna 3, be provided with between directional aviation antenna 4 with surface orientation antenna 3 directional aviation antenna 4 and/or surface orientation antenna 3 can be made freely to rotate thus make directional aviation antenna 4 towards with surface orientation antenna 3 towards ACU antenna control unit mutually corresponding all the time, preferably, here directional aviation antenna 4 and surface orientation antenna 3 synchronous axial system, so no matter airborne vehicle 2 is in any position, directional aviation antenna 4 and surface orientation antenna 3 all can be mutually corresponding, thus the gamut realizing directional antenna covers.
Particularly, ACU antenna control unit in the present embodiment comprise to be arranged between ground station's support body 1 and surface orientation antenna 3 and can according to directional aviation antenna 4 position adjust surface orientation antenna 3 towards thus make surface orientation antenna 3 point to the ground-plane antenna adjust structure 5 of directional aviation antenna 4, be provided with between airborne vehicle 2 and directional aviation antenna 4 can according to ground directional antenna 3 position adjust directional aviation antenna 4 towards thus make directional aviation antenna 4 point to the aerodiscone antenna adjust structure 6 of surface orientation antenna 3, make like this surface orientation antenna 3 and directional aviation antenna 4 can respectively according to the position of the other side adjust self towards thus make that surface orientation antenna 3 and directional aviation antenna 4 are mutually corresponding all the time to be arranged.
As in Figure 2-4, here ground-plane antenna adjust structure 5 comprises circumference and rotates the first housing 51 being arranged on ground station's support body 1 upper end, surface orientation antenna 3 is hinged is arranged on the first housing 51 upper end, first housing 51 is different with the activity direction that surface orientation antenna 3 is hinged and connected with the first housing 51 from the rotation direction that ground station support body 1 is rotatedly connected, be provided with between first housing 51 and ground station's support body 1 and can make the first housing 51 first circumferential rotating drive mechanism 52 of rotating circumferential relative to ground station's support body 1, first swing driving mechanism 53 that surface orientation antenna 3 can be made relative to the first housing 51 circuit oscillation is provided with between first housing 51 and surface orientation antenna 3, first circumferential rotating drive mechanism 52 and the first swing driving mechanism 53 are connected with the MPU module 54 be arranged in the first housing 51 respectively, one MPU module 54 is connected with the first GPS module 55 be arranged in the first housing 51, and a MPU module 54 and the first GPS module 55 are all connected with the first supply module 56 be arranged in the first housing 51, first housing 51 is provided with the display module 57 be connected with a MPU module 54, namely the first GPS module 55 is here for determining ground directional antenna 3 position, one MPU module 54 obtains the first GPS module 55 information and sends to directional aviation antenna 4, here surface orientation antenna 3 and directional aviation antenna 4 are bidirectional data transfers, one MPU module 54 makes the first circumferential rotating drive mechanism 52 and the first swing driving mechanism 53 adjust the angle of surface orientation antenna 3, make it all the time towards directional aviation antenna 4.
Preferably, in the present embodiment first circumferential rotating drive mechanism 52 comprises the support 521 being arranged on ground station's support body 1 upper end, the first rotational drive motor 522 be connected with a MPU module 54 is provided with between support 521 with the first housing 51, first rotational drive motor 522 is arranged on support 521 or the first housing 51, and the output shaft of the first rotational drive motor 522 and the first housing 51 or support 521 are fixedly linked; Ground station's support body 1 comprises at least three bodies of rod 11, and the body of rod 11 one end crosses and is all connected with support 521, and the body of rod 11 other end is tilted to down respectively and circumference is uniformly distributed setting; First rotational drive motor 522 is stepping motor or brushless electric machine, and namely the first rotational drive motor 522 here drives surface orientation antenna 3 circumference rotate thus realize the adjustment of surface orientation antenna 3 circumferential position.Here the first swing driving mechanism 53 comprises the first installing rack 531 rotating and be arranged on the first housing 51 upper end, surface orientation antenna 3 is arranged on the first installing rack 531, and be provided with the first wobble component assembly that can drive the first installing rack 531 circuit oscillation between the first installing rack 531 and the first housing 51, wherein, here the first wobble component assembly comprises two correspondences and to be arranged in the first housing 51 and be all connected with a MPU module 54 first to drive steering wheel 532, first drives the output shaft of steering wheel 532 to pass the first housing 51 respectively, first installing rack 531 two ends are bent to form the first installation portion 533 respectively outside the first housing 51, and the first installation portion 533 drives the output shaft of steering wheel 532 to be connected with first respectively, first installing rack 531 is in bending, and in the middle part of the first installing rack 531, there is outward extending location division 534, and surface orientation antenna 3 is arranged on location division 534, namely steering wheel 532 is driven to adjust surface orientation antenna 3 pendulum angle by first, the adjustment of combined ground directional antenna 3 circumferential position thus realize surface orientation antenna 3 universal position adjustment.
Further, as shown in Fig. 2 and Fig. 5-8, here aerodiscone antenna adjust structure 6 comprises circumference and rotates the second housing 61 being arranged on airborne vehicle 2 bottom side, directional aviation antenna 4 is hinged to be arranged on the second housing 61 and directional aviation antenna 4 is tilted to lower setting on rear side of airborne vehicle 2 body, be provided with between second housing 61 and airborne vehicle 2 and can make the second housing 61 relative to the circumferential second week rotated of airborne vehicle 2 to rotating drive mechanism 62, second swing driving mechanism 63 that directional aviation antenna 4 can be made to swing relative to the second housing 61 is provided with between second housing 61 and directional aviation antenna 4, second week is connected with the 2nd MPU module 64 be arranged in the second housing 61 to rotating drive mechanism 62 respectively with the second swing driving mechanism 63,2nd MPU module 64 with to be arranged in the second housing 61 and to be connected with the second GPS module 65 that the first GPS module 55 matches, and the 2nd MPU module 64 and the second GPS module 65 are all connected with the second supply module 66 be arranged in the second housing 61, namely the second GPS module 65 is here for determining directional aviation antenna 4 position, 2nd MPU module 64 obtains the second GPS module 65 information and sends to surface orientation antenna 3, here surface orientation antenna 3 and directional aviation antenna 4 are bidirectional data transfers, 2nd MPU module 64 makes second week adjust the angle of directional aviation antenna 4 to rotating drive mechanism 62 and the second swing driving mechanism 63, make it all the time towards surface orientation antenna 3.
Wherein, here second week comprises the Connection Block 621 be arranged in the middle part of airborne vehicle 2 bottom side to rotating drive mechanism 62, the second rotational drive motor 622 be connected with the 2nd MPU module 64 is provided with between Connection Block 621 with the second housing 61, second rotational drive motor 622 is arranged on Connection Block 621 or the second housing 61, and the output shaft of the second rotational drive motor 622 and the second housing 61 or Connection Block 621 are fixedly linked; Airborne vehicle 2 is any one or multiple combination in unmanned plane, dirigible and balloon; Second rotational drive motor 622 is stepping motor or brushless electric machine, and namely the second rotational drive motor 622 here drives directional aviation antenna 4 circumference rotate thus realize the adjustment of directional aviation antenna 4 circumferential position.
Secondly, here the second swing driving mechanism 63 comprises and is hingedly arranged on the second housing 61 upper end and sweeping second installing rack 631, directional aviation antenna 4 is arranged in the middle part of the second installing rack 631, and be provided with the second wobble drive assembly that can drive the second installing rack 631 circuit oscillation between the second installing rack 631 and the second housing 61, preferably, here the second wobble drive assembly comprises two correspondences and to be arranged in the second housing 61 and be all connected with the 2nd MPU module 64 second to drive steering wheel 632, second drives the output shaft of steering wheel 632 to pass the second housing 61 respectively, second installing rack 631 two ends are bent to form the second installation portion 633 respectively outside the second housing 61, and the second installation portion 633 drives the output shaft of steering wheel 632 to be connected with second respectively, namely steering wheel 632 is driven to adjust directional aviation antenna 4 pendulum angle by second, in conjunction with directional aviation antenna 4 circumferential position adjustment thus realize directional aviation antenna universal 4 positions adjustment.
The principle of the present embodiment is: by the first GPS module 55 for determining ground directional antenna 3 position, one MPU module 54 obtains the first GPS module 55 information and sends to directional aviation antenna 4, here surface orientation antenna 3 and directional aviation antenna 4 are bidirectional data transfers, one MPU module 54 makes the first driving steering wheel 532 to adjust surface orientation antenna 3 pendulum angle and to drive surface orientation antenna 3 circumference rotate thus realize the adjustment of surface orientation antenna 3 circumferential position by realizing the first rotational drive motor 522, thus realize surface orientation antenna 3 universal position adjustment, make it all the time towards directional aviation antenna 4, by the second GPS module 65 for determining directional aviation antenna 4 position, 2nd MPU module 64 obtains the second GPS module 65 information and sends to surface orientation antenna 3, here surface orientation antenna 3 and directional aviation antenna 4 are bidirectional data transfers, 2nd MPU module 64 makes the second rotational drive motor 622 drive directional aviation antenna 4 circumference to rotate and drive steering wheel 632 to adjust directional aviation antenna 4 pendulum angle by second, thus realize the universal 4 position adjustment of directional aviation antenna, make it all the time towards surface orientation antenna 3.
Specific embodiment described herein is only to the explanation for example of the utility model spirit.The utility model person of ordinary skill in the field can make various amendment or supplements or adopt similar mode to substitute to described specific embodiment, but can't depart from spirit of the present utility model or surmount the scope that appended claims defines.
Although more employ ground station's support body 1 herein, the body of rod 11, airborne vehicle 2, surface orientation antenna 3, directional aviation antenna 4, ground-plane antenna adjust structure 5, first housing 51, first circumferential rotating drive mechanism 52, support 521, first rotational drive motor 522, first swing driving mechanism 53, first installing rack 531, first drives steering wheel 532, first installation portion 533, location division 534, one MPU module 54, first GPS module 55, first supply module 56, display module 57, aerodiscone antenna adjust structure 6, second housing 61, second week is to rotating drive mechanism 62, Connection Block 621, second rotational drive motor 622, second swing driving mechanism 63, second installing rack 631, second drives steering wheel 632, second installation portion 633, 2nd MPU module 64, second GPS module 65, second term such as supply module 66 grade, but do not get rid of the possibility using other term.These terms are used to be only used to describe and explain essence of the present utility model more easily; The restriction that they are construed to any one additional is all contrary with the utility model spirit.
Claims (10)
1. a gamut beam aerial system, comprise ground station's support body (1) and airborne vehicle (2), it is characterized in that, described ground station's support body (1) has the surface orientation antenna (3) of at least one activity direction, described airborne vehicle (2) has at least one activity direction put and the directional aviation antenna (4) of bidirectional data transfers can be carried out with surface orientation antenna (3), described directional aviation antenna (4) be provided with between surface orientation antenna (3) directional aviation antenna (4) and/or surface orientation antenna (3) can be made freely to rotate thus make directional aviation antenna (4) towards with surface orientation antenna (3) towards ACU antenna control unit mutually corresponding all the time.
2. gamut beam aerial system according to claim 1, it is characterized in that, described ACU antenna control unit comprise to be arranged between ground station's support body (1) and surface orientation antenna (3) and can according to directional aviation antenna (4) position adjust surface orientation antenna (3) towards thus make surface orientation antenna (3) point to the ground-plane antenna adjust structure (5) of directional aviation antenna (4), be provided with between described airborne vehicle (2) and directional aviation antenna (4) can according to ground directional antenna (3) position adjust directional aviation antenna (4) towards thus make directional aviation antenna (4) point to the aerodiscone antenna adjust structure (6) of surface orientation antenna (3).
3. gamut beam aerial system according to claim 2, it is characterized in that, described ground-plane antenna adjust structure (5) comprises circumference and rotates the first housing (51) being arranged on ground station's support body (1) upper end, described surface orientation antenna (3) is hinged is arranged on the first housing (51) upper end, described the first housing (51) is different with the activity direction that surface orientation antenna (3) is hinged and connected with the first housing (51) from the rotation direction that ground station's support body (1) is rotatedly connected, be provided with between described the first housing (51) and ground station's support body (1) and the first housing (51) first circumferential rotating drive mechanism (52) of rotating circumferential relative to ground station's support body (1) can be made, first swing driving mechanism (53) that surface orientation antenna (3) can be made relative to the first housing (51) circuit oscillation is provided with between described the first housing (51) and surface orientation antenna (3), described first circumferential rotating drive mechanism (52) and the first swing driving mechanism (53) are connected with the MPU module (54) be arranged in the first housing (51) respectively, a described MPU module (54) is connected with the first GPS module (55) be arranged in the first housing (51), and a described MPU module (54) is all connected with the first supply module (56) be arranged in the first housing (51) with the first GPS module (55), first housing (51) is provided with the display module (57) be connected with a MPU module (54).
4. gamut beam aerial system according to claim 3, it is characterized in that, described first circumferential rotating drive mechanism (52) comprises the support (521) being arranged on ground station's support body (1) upper end, described support (521) be provided with the first rotational drive motor (522) be connected with a MPU module (54) between the first housing (51), described the first rotational drive motor (522) is arranged on support (521) or the first housing (51), and the output shaft of described the first rotational drive motor (522) and the first housing (51) or support (521) are fixedly linked, described ground station's support body (1) comprises at least three bodies of rod (11), the described body of rod (11) one end crosses and is all connected with support (521), and the described body of rod (11) other end is tilted to down respectively and circumference is uniformly distributed setting, described the first rotational drive motor (522) is stepping motor or brushless electric machine.
5. gamut beam aerial system according to claim 4, it is characterized in that, described the first swing driving mechanism (53) comprises the first installing rack (531) that rotation is arranged on the first housing (51) upper end, described surface orientation antenna (3) is arranged on the first installing rack (531), and is provided with the first wobble component assembly that can drive the first installing rack (531) circuit oscillation between described the first installing rack (531) and the first housing (51).
6. gamut beam aerial system according to claim 5, it is characterized in that, the first described wobble component assembly comprises two correspondences and to be arranged in the first housing (51) and be all connected with a MPU module (54) first to drive steering wheel (532), described first drives the output shaft of steering wheel (532) to pass the first housing (51) respectively, described the first installing rack (531) two ends are bent to form the first installation portion (533) towards the first housing (51) outside respectively, and described the first installation portion (533) drives the output shaft of steering wheel (532) to be connected respectively with first, described the first installing rack (531) is in bending, and described the first installing rack (531) middle part has outward extending location division (534), and described surface orientation antenna (3) is arranged on location division (534).
7. the gamut beam aerial system according to claim 3 or 4 or 5 or 6, it is characterized in that, described aerodiscone antenna adjust structure (6) comprises circumference and rotates the second housing (61) being arranged on airborne vehicle (2) bottom side, described directional aviation antenna (4) is hinged to be arranged on the second housing (61) upper and described directional aviation antenna (4) on rear side of airborne vehicle (2) body and to be tilted to lower setting, be provided with between described the second housing (61) and airborne vehicle (2) and the second housing (61) can be made relative to the circumferential second week rotated of airborne vehicle (2) to rotating drive mechanism (62), second swing driving mechanism (63) that directional aviation antenna (4) can be made to swing relative to the second housing (61) is provided with between described the second housing (61) and directional aviation antenna (4), described second week is connected with the 2nd MPU module (64) be arranged in the second housing (61) to rotating drive mechanism (62) respectively with the second swing driving mechanism (63), the 2nd described MPU module (64) with to be arranged in the second housing (61) and to be connected with the second GPS module (65) that the first GPS module (55) matches, and the 2nd described MPU module (64) is all connected with the second supply module (66) be arranged in the second housing (61) with the second GPS module (65).
8. gamut beam aerial system according to claim 7, it is characterized in that, described second week comprises the Connection Block (621) be arranged in the middle part of airborne vehicle (2) bottom side to rotating drive mechanism (62), described Connection Block (621) be provided with the second rotational drive motor (622) be connected with the 2nd MPU module (64) between the second housing (61), described the second rotational drive motor (622) is arranged on Connection Block (621) or the second housing (61), and the output shaft of described the second rotational drive motor (622) and the second housing (61) or Connection Block (621) are fixedly linked, described airborne vehicle (2) is unmanned plane, any one or multiple combination in dirigible and balloon, described the second rotational drive motor (622) is stepping motor or brushless electric machine.
9. gamut beam aerial system according to claim 8, it is characterized in that, described the second swing driving mechanism (63) comprises and is hingedly arranged on the second housing (61) upper end and sweeping second installing rack (631), described directional aviation antenna (4) is arranged on the second installing rack (631) middle part, and is provided with the second wobble drive assembly that can drive the second installing rack (631) circuit oscillation between described the second installing rack (631) and the second housing (61).
10. gamut beam aerial system according to claim 9, it is characterized in that, the second described wobble drive assembly comprises two correspondences and to be arranged in the second housing (61) and be all connected with the 2nd MPU module (64) second to drive steering wheel (632), described second drives the output shaft of steering wheel (632) to pass the second housing (61) respectively, described the second installing rack (631) two ends are bent to form the second installation portion (633) towards the second housing (61) outside respectively, and described the second installation portion (633) drives the output shaft of steering wheel (632) to be connected respectively with second.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520729508.5U CN205069857U (en) | 2015-09-20 | 2015-09-20 | Gamut directional antenna system |
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|---|---|---|---|
| CN201520729508.5U CN205069857U (en) | 2015-09-20 | 2015-09-20 | Gamut directional antenna system |
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| CN205069857U true CN205069857U (en) | 2016-03-02 |
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| CN201520729508.5U Expired - Fee Related CN205069857U (en) | 2015-09-20 | 2015-09-20 | Gamut directional antenna system |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105119041A (en) * | 2015-09-20 | 2015-12-02 | 金华技物光电研究所有限公司 | Full scope directional antenna system |
| CN105892492A (en) * | 2016-06-07 | 2016-08-24 | 南方科技大学 | Unmanned aerial vehicle communication control method and device |
| CN106602219A (en) * | 2016-11-04 | 2017-04-26 | 北京佰才邦技术有限公司 | Antenna direction adjusting method and device |
| WO2018094625A1 (en) * | 2016-11-23 | 2018-05-31 | 深圳市大疆创新科技有限公司 | Frame of unmanned aerial vehicle, unmanned aerial vehicle and antenna switching method |
| WO2018098768A1 (en) * | 2016-12-01 | 2018-06-07 | 深圳市大疆创新科技有限公司 | Method for tracking directional antenna, and communication device |
| CN108513646A (en) * | 2017-06-29 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Control method, unmanned plane and computer readable storage medium |
| CN110931977A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
| CN110931976A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
| CN110931978A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
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| CN113541743A (en) * | 2020-12-17 | 2021-10-22 | 中兴通讯股份有限公司 | Ground-to-air communication control method, antenna, base station and storage medium |
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2015
- 2015-09-20 CN CN201520729508.5U patent/CN205069857U/en not_active Expired - Fee Related
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| CN105119041B (en) * | 2015-09-20 | 2017-10-31 | 金华技物光电研究所有限公司 | Gamut beam aerial system |
| CN105119041A (en) * | 2015-09-20 | 2015-12-02 | 金华技物光电研究所有限公司 | Full scope directional antenna system |
| CN105892492A (en) * | 2016-06-07 | 2016-08-24 | 南方科技大学 | Unmanned aerial vehicle communication control method and device |
| CN106602219A (en) * | 2016-11-04 | 2017-04-26 | 北京佰才邦技术有限公司 | Antenna direction adjusting method and device |
| WO2018094625A1 (en) * | 2016-11-23 | 2018-05-31 | 深圳市大疆创新科技有限公司 | Frame of unmanned aerial vehicle, unmanned aerial vehicle and antenna switching method |
| US10978799B2 (en) | 2016-12-01 | 2021-04-13 | SZ DJI Technology Co., Ltd. | Directional antenna tracking method and communication device |
| WO2018098768A1 (en) * | 2016-12-01 | 2018-06-07 | 深圳市大疆创新科技有限公司 | Method for tracking directional antenna, and communication device |
| CN108513646A (en) * | 2017-06-29 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Control method, unmanned plane and computer readable storage medium |
| WO2019000345A1 (en) * | 2017-06-29 | 2019-01-03 | 深圳市大疆创新科技有限公司 | Control method, unmanned aerial vehicle, and computer readable storage medium |
| CN110931977A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
| CN110931976A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
| CN110931978A (en) * | 2019-11-22 | 2020-03-27 | Oppo广东移动通信有限公司 | Antenna unit and client terminal device |
| CN111106448A (en) * | 2019-11-22 | 2020-05-05 | Oppo广东移动通信有限公司 | Client terminal device |
| CN113541743A (en) * | 2020-12-17 | 2021-10-22 | 中兴通讯股份有限公司 | Ground-to-air communication control method, antenna, base station and storage medium |
| WO2022127626A1 (en) * | 2020-12-17 | 2022-06-23 | 中兴通讯股份有限公司 | Air-ground communication control method, and antenna, base station and storage medium |
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