A portable integrated satellite communication terminal

Abstract

The portable integrated satellite communication terminal of the present invention comprises an upper module, a middle module and a base, and integrates electrical components such as a flat antenna, a transceiver, an inclinometer, an antenna control unit, a digital baseband unit, a carrier receiver, a GPS receiving module or a GPS / BD dual-mode receiving module, a power distribution unit and an electronic compass in a small box. The transceiver integrates BUC and LNB, and the antenna control unit controls the pitch motor to adjust the angle of the upper support relative to the middle support according to the position information obtained by the GPS receiving module, and controls the pitch motor to adjust the rotation angle of the middle support relative to the base, so as to realize automatic adjustment of the pitch angle and heading angle. The satellite communication terminal of the present invention adopts an integrated design, which is convenient for users to carry and collect.

Description

Technical Field

[0001] The present invention relates to the technical field of satellite communication terminals, and in particular to a portable integrated satellite communication terminal. Background Art

[0002] Satellite communication user stations are an important part of satellite communication systems. Among them, portable satellite communication user stations (including antennas, RF front ends and satellite communication terminals) have become the most common form of user stations due to their small size, low cost and ease of use. They are widely used in public security fire fighting, emergency communications, resource exploration and other fields.

[0003] Traditional satellite communication terminals do not include equipment such as antennas and RF front-ends. In the field of emergency communications, they are generally used in conjunction with portable satellite antennas. Portable satellite antennas generally take the form of parabolic antennas, which work with BUC and LNB to form the antenna feed equipment of a portable user station. This type of parabolic antenna generally has multiple panels on the antenna surface. When in use, they need to be spliced ​​and then installed with components such as brackets, feeds, BUC (Block Up-Converter, up-conversion power amplifier and LNB (Low Noise Block, high-frequency head), and finally use cables to connect the antenna and satellite communication terminal before use. In addition, due to the irregular shapes of the various accessories of the antenna, it is also very inconvenient to store them. This type of equipment often requires one or two suitcases for storage and transportation. Summary of the invention

[0004] The purpose of the present invention is to solve the deficiencies of the prior art and provide a portable integrated satellite communication terminal.

[0005] The technical solution of the present invention is as follows:

[0006] A portable integrated satellite communication terminal, comprising:

[0007] The upper module includes an upper support, and a radome, a flat antenna, a transceiver and an inclinometer mounted thereon, the transceiver integrates a BUC and an LNB, the radome is mounted on the upper side of the upper support, the flat antenna, the transceiver and the inclinometer are mounted in the radome, the transmitting port of the transceiver is connected to the transmitting port of the flat antenna, and the receiving port of the transceiver is connected to the receiving port of the flat antenna;

[0008] The middle-layer module includes a middle-layer support, and an antenna control unit, a digital baseband unit, a carrier receiver, a GPS receiving module or a GPS / BD dual-mode receiving module, and an electronic compass installed thereon. The rear side of the upper-layer support is connected to the middle-layer support. The intermediate frequency input of the carrier receiver is connected to the intermediate frequency receiving of the transceiver, the intermediate frequency output of the carrier receiver is connected to the intermediate frequency receiving input of the digital baseband, and the intermediate frequency transmitting of the digital baseband is connected to the intermediate frequency transmitting of the transceiver. The antenna control unit is respectively connected to the inclinometer, the carrier receiver, the GPS receiving module, and the electronic compass.

[0009] A base, rotatably connected to the lower side of the middle support;

[0010] The pitch motor is installed on the middle support or the upper support and is connected to the antenna control unit. The pitch motor drives the upper support to move relative to the middle support through the pitch transmission assembly to adjust the pitch angle.

[0011] The heading motor is installed on the middle-level support or base and is connected to the antenna control unit. The pitch motor drives the middle-level support to rotate relative to the base through the heading transmission assembly to adjust the heading angle.

[0012] The communication terminal of the present invention has the following advantages:

[0013] 1. It adopts a three-layer structure of upper, middle and lower layers. The flat antenna and transceiver are installed in the upper support, and the signal processing units are installed in the middle support. The communication function and electromechanical control function adopt an integrated design. It can be used and stored without installing any accessories, which improves portability and ease of use.

[0014] 2. The use of flat antennas makes the device more regular in shape and smaller in size compared to traditional parabolic antennas;

[0015] 3. The RF module uses a transceiver with integrated BUC and LNB, which does not require assembly and wiring. The opening and closing time is shorter, the equipment is more compact, and the use area and storage volume are smaller. The layout of each module is designed and integrated, which solves the problems of traditional portable satellite communication terminals with many components, large storage volume and complex operation, and is more convenient for collection and carrying.

[0016] 4. After powering on, the antenna control unit controls the pitch motor to adjust the angle of the upper support relative to the middle support according to the location information obtained by the GPS receiving module, and controls the pitch motor to adjust the rotation angle of the middle support relative to the base, so as to automatically adjust the pitch angle and heading angle, and realize automatic satellite alignment.

[0017] 5. During the adjustment of the antenna attitude (pitch angle and heading angle), the electronic compass and inclinometer play a role in angle data value feedback, forming a closed-loop control and improving the adjustment accuracy.

[0018] There are two ways to install the pitch motor. One is to install it on the middle support. The pitch transmission assembly includes a first gear and a second gear. The first gear is connected to the pitch motor, and the second gear is fixedly connected to the upper support. The first gear and the second gear are meshed for transmission. The second is to install it on the upper support. The pitch transmission assembly includes a first gear and a second gear. The first gear is connected to the pitch motor, and the second gear is fixedly connected to the middle support. The first gear and the second gear are meshed for transmission. Preferably, the pitch motor is installed on the middle support, so that the pitch motor and the pitch transmission assembly can be integrated in the middle module, which is convenient for circuit design and electrical component layout, and at the same time allows the upper module to have more space for arranging the transceiver module.

[0019] There are two ways to install the heading motor. One is to install it on the middle-level support. The heading transmission assembly includes a third gear and a fourth gear. The third gear is connected to the heading motor. The middle part of the middle-level support is rotatably connected to the middle part of the base. The fourth gear is coaxially arranged with the rotation axis of the middle-level support and the base. The fourth gear is fixedly connected to the base. The third gear and the fourth gear are meshed for transmission. The second is to install it on the base. The heading transmission assembly includes a third gear and a fourth gear. The third gear is connected to the heading motor. The middle part of the middle-level support is rotatably connected to the middle part of the base. The fourth gear is coaxially arranged with the rotation axis of the middle-level support and the base. The fourth gear is fixedly connected to the middle-level support. The third gear and the fourth gear are meshed for transmission. Preferably, the heading motor is installed on the middle-level support, which better protects the heading motor and simplifies the structure of the base.

[0020] Preferably, the fourth gear is a toothed disc, the middle of which is provided with a middle hole, and the middle of the middle support is connected to the middle of the base through a bearing. The toothed disc has a large bearing capacity and a stable transmission.

[0021] Preferably, the flat panel antenna is a flat panel array antenna, and the transceiver and the inclinometer are installed on the lower side of the flat panel array antenna. The use of a flat panel array antenna can further reduce the diameter of the antenna and the volume of the device.

[0022] Furthermore, the antenna cover is provided with an antenna accommodating cavity with an opening at the bottom, the upper support is provided with an upper component chamber with an opening at the top, the flat antenna is installed in the antenna accommodating cavity, and the transceiver and the inclinometer are installed in the upper component chamber. By providing the upper component chamber, the above-mentioned electronic components can be better protected, and the product can be more integrated and the volume of the equipment can be reduced.

[0023] Preferably, the middle support is provided with a middle component room with an upper opening, and the antenna control unit, the digital baseband unit, the carrier receiver, the GPS receiving module, the power distribution unit and the electronic compass are installed in the middle component room. The electronic components are installed in the middle component room, so that each electronic component can be better protected, and the product can be more integrated and the volume of the equipment can be reduced.

[0024] Preferably, the upper support can be placed in the middle component room when stored, and the lower end of the antenna cover wall matches the upper end of the middle support in shape, so that the lower end of the antenna cover wall and the upper end of the middle support are spliced ​​together when stored. By setting it in this way, the upper support can be stored between the antenna cover and the middle support when stored, further improving the integration of the product and making the volume of the device smaller when stored.

[0025] Preferably, it also includes a power distribution unit, which is connected to an external power source or a built-in battery module, and provides power for each component module on the middle layer module, as well as the pitch motor and the heading motor.

[0026] Preferably, the middle support is provided with a rechargeable battery module, and the battery module is electrically connected to the power distribution unit. By having a built-in rechargeable battery module, the terminal does not rely on external power supply. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Figure 1 Schematic diagram of the storage state of the integrated satellite communication terminal of the present invention

[0028] Figure 2 Schematic diagram of the integrated satellite communication terminal after adjusting the heading angle of the present invention

[0029] Figure 3 The integrated satellite communication terminal of the present invention is schematically shown after adjusting the heading angle and pitch angle. Figure 1

[0030] Figure 4 The integrated satellite communication terminal of the present invention is schematically shown after adjusting the heading angle and pitch angle. Figure 2

[0031] Figure 5 An exploded view of the upper module of the integrated satellite communication terminal of the present invention

[0032] Figure 6 A bottom view of the upper module of the integrated satellite communication terminal of the present invention (with the upper support removed)

[0033] Figure 7 Schematic diagram of the middle module of the integrated satellite communication terminal of the present invention

[0034] Figure 8 A bottom view of the middle module of the integrated satellite communication terminal of the present invention

[0035] Fig. 9 A schematic diagram of the base of the integrated satellite communication terminal of the present invention

[0036] Fig.10 A diagram showing the relationship between the components of the present invention DETAILED DESCRIPTION

[0037] A preferred technical solution of the present invention is described below in conjunction with the accompanying drawings:

[0038] See also Figures 1 to 10 The portable integrated satellite communication terminal includes an upper module 1, a middle module 2 and a base 3.

[0039] The upper module 1 includes an upper support 100, and a radome 101, a flat antenna 102, a transceiver 103 and an inclinometer 104 mounted thereon. The transceiver 103 integrates a BUC and an LNB. The radome 101 is mounted on the upper side of the upper support 100, and the flat antenna 102, the transceiver 103 and the inclinometer 104 are mounted in the radome 101. The transmitting port of the transceiver 103 is connected to the transmitting port of the flat antenna 102 through a waveguide 1021, and the receiving port of the transceiver 103 is connected to the receiving port of the flat antenna 102 after being connected to a waveguide filter (not shown) through a waveguide 1022.

[0040] The middle layer module 2 includes a middle layer support 200 and an antenna control unit 201 installed thereon, a digital baseband unit 202, a carrier receiver 203, a GPS receiving module 204, a power distribution unit 205, an electronic compass 206, a pitch motor 207 and a heading motor 208. The rear side of the upper layer support 100 is connected to the middle layer support 200. The intermediate frequency input of the carrier receiver 203 is connected to the intermediate frequency receiving of the transceiver 103, the intermediate frequency output of the carrier receiver 203 is connected to the intermediate frequency receiving input of the digital baseband 202, and the intermediate frequency transmitting of the digital baseband 202 is connected to the intermediate frequency transmitting of the transceiver 103. The antenna control unit 201 is respectively connected to the inclinometer 104, the carrier receiver 203, the GPS receiving module 204 and the electronic compass 206 (and the pitch driver 208) through a plurality of control ports. 71 and a heading driver 2081), the pitch motor 207 is connected to the antenna control unit 201, and the pitch motor 207 drives the upper support 100 to move relative to the middle support 100 through the pitch transmission component 2070 to adjust the pitch angle; the heading motor 208 is connected to the antenna control unit 201, and the pitch motor 208 drives the middle support 200 to rotate relative to the base 3 through the heading transmission component 2080 to adjust the heading angle, the power distribution unit 205 is connected to an external power supply or a built-in battery module, and the power distribution unit 205 provides power for the antenna control unit 201, the digital baseband unit 202, the carrier receiver 203, the GPS receiving module 204, the power distribution unit 205, the electronic compass 206, the pitch motor 207 and the heading motor 208 on the middle module 2.

[0041] In addition, the antenna control unit 201, digital baseband unit 202, carrier receiver 203, GPS receiving module 204, power distribution unit 205, electronic compass 206, pitch motor 207 and heading motor 208 in the middle module 2 can adopt a tiled layout or a partially stacked layout.

[0042] Specifically, the connections between the upper module 1 and the middle module 2 are such that the IF interface of the transceiver 103 leads to a coaxial cable connected to the IF interface of the digital baseband 202 , and the inclinometer 104 leads to a control cable connected to the antenna control unit 201 .

[0043] The base 3 is rotatably connected to the lower side of the middle support 200 .

[0044] Preferably, the transceiver 103 adopts an integrated BUC and LNB design, is designed as a rectangular parallelepiped structure, provides two waveguide interfaces on the side for connecting to the flat antenna 102, and provides two interfaces for connecting to the digital baseband unit 202.

[0045] Preferably, the middle support 201 is provided with a rechargeable battery module, and the battery module is electrically connected to the power distribution unit 205. By having a built-in rechargeable battery module, the terminal does not rely on external power supply.

[0046] Preferably, when the RF operating bandwidth exceeds the range of the IF operating bandwidth, the transceiver 103 adopts a multi-local oscillator signal design, and switches the local oscillator of the transceiver 103 by modulating a low-frequency FSK control signal on the IF signal.

[0047] If the digital baseband unit 202 provides a carrier receiving signal strength that meets the performance requirements and provides closed-loop control information to the antenna control unit 201, the carrier receiver 203 can be eliminated.

[0048] In addition, the present invention is also provided with a human-computer interaction interface with a display panel.

[0049] See also Figure 4 and Figure 7 The pitch transmission assembly 2070 includes a first gear 20701 and a second gear 20702. The first gear 20701 is connected to the pitch motor 207, and the second gear 20702 is fixedly connected to the upper support 100. The first gear 20701 and the second gear 20702 are meshed for transmission.

[0050] The pitch motor 207 is installed on the middle support 200, so that the pitch motor 207 and the pitch transmission assembly 2070 can be integrated in the middle module 2, which is convenient for circuit design and electrical component layout, and at the same time allows the upper module 1 to have more space for arranging the transceiver module.

[0051] Alternatively, the pitch motor 207 may also be installed on the upper support 100, and the pitch transmission assembly 2070 includes a first gear 20701 and a second gear 20702, wherein the first gear 20701 is connected to the pitch motor 207, and the second gear 20702 is fixedly connected to the middle support 200, and the first gear 20701 and the second gear 20702 are engaged for transmission.

[0052] See also Figures 7 to 9 The heading transmission assembly 2080 includes a third gear 20801 and a fourth gear 20802, the third gear 20801 is connected to the heading motor 208, the middle part of the middle support 200 is rotatably connected to the middle part of the base 3, the fourth gear 20802 is coaxially arranged with the rotation axis of the middle support 200 and the base 3, the fourth gear 20802 is fixedly connected to the base 3, and the third gear 20801 and the fourth gear 20802 are meshed for transmission. Preferably, the heading motor 208 is installed on the middle support 200, which better protects the heading motor 208 and simplifies the structure of the base 3.

[0053] Alternatively, the heading motor 208 can be installed on the base 3, and the heading transmission assembly 2080 includes a third gear 20801 and a fourth gear 20802, the third gear 20801 is connected to the heading motor 208, the middle part of the middle support 200 is rotatably connected to the middle part of the base 3, the fourth gear 20802 is coaxially arranged with the rotation axis of the middle support 200 and the base 3, the fourth gear 20802 is fixedly connected to the lower side of the middle support 200, and the third gear 20801 and the fourth gear 20802 are engaged for transmission.

[0054] The fourth gear 20802 is a toothed disc, and a center hole 2081 is provided in the middle thereof. The middle part of the middle support 200 and the middle part of the base 3 are rotatably connected through the center hole 2081. The toothed disc has a large bearing capacity and a stable transmission.

[0055] The middle part of the middle support 200 is connected to the middle part of the base 300 through the bearing 2082. Specifically, the inner ring of the bearing 2082 is fixedly connected to the middle part of the base 3, and the outer ring of the bearing 2082 is fixedly connected to the middle part of the middle support 200; or, the outer ring of the bearing 2082 is fixedly connected to the middle part of the base 3, and the inner ring of the bearing 2082 is fixedly connected to the middle part of the middle support 200.

[0056] See also Figure 7, and also includes a pitch motor driving module 2071 and a heading motor driving module 2081. The pitch motor driving module 2071 is connected to the pitch motor 207 and the antenna control unit 201, and the heading motor driving module 2081 is connected to the heading motor 208 and the antenna control unit 201. The pitch angle adjustment signal and the heading angle adjustment signal sent by the antenna control unit 201 drive the corresponding pitch motor 207 and the heading motor 208 to adjust the angle respectively through the pitch motor driving module 2071 and the heading motor driving module 2081.

[0057] See 4 and Figure 5 The antenna cover 101 is provided with an antenna accommodating cavity 1011 with an opening at the bottom, the upper support 100 is provided with an upper component chamber 1001 with an opening at the top, the flat antenna 102 is installed in the antenna accommodating cavity 1011, and the transceiver 103 and the inclinometer 104 are installed in the upper component chamber 1001. By providing the upper component chamber 1001, the flat antenna 1001, the transceiver 103 and the inclinometer 104 are installed in the space between the upper component chamber 1001 and the antenna accommodating cavity 1011, so that the above-mentioned electronic components can be better protected, and at the same time, the product can be more integrated and the volume of the equipment can be reduced.

[0058] See also Figure 4 and Figure 7 The middle support 200 is provided with a middle component chamber 2001 with an upper opening, and a digital baseband unit 202, a carrier receiver 203, a GPS receiving module 204, a power distribution unit 205, an electronic compass 206, a pitch motor 207 and a heading motor 208 are installed in the middle component chamber 2001. The above electronic components are installed in the middle component chamber 2001, so that the above electronic components can be better protected, and the product can be more integrated and the volume of the equipment can be reduced.

[0059] Furthermore, the upper support 100 can be placed in the middle component chamber 2001 when stored, and the lower end of the peripheral wall of the antenna cover 101 matches the upper end of the middle support 200 in shape, so that the lower end of the peripheral wall of the antenna cover 101 is combined with the upper end of the middle support 200 when stored. By setting it in this way, the upper support 100 can be stored between the antenna cover 101 and the middle support 200 when stored, further improving the integration of the product and making the volume of the device smaller when stored.

[0060] See also Figure 5 and Figure 6The flat panel antenna 102 is a flat panel array antenna, and the transceiver 103 and the inclinometer 104 are installed on the lower side of the flat panel antenna 102. The flat panel array antenna can further reduce the diameter of the antenna and reduce the volume of the device. Specifically, the flat panel antenna 102 adopts a waveguide horn array antenna, which is designed in a rectangular parallelepiped shape. The horns arranged vertically and horizontally constitute the radiation surface of the antenna, that is, the upper surface of the flat panel antenna 102. Two waveguide interfaces are provided on the lower surface of the flat panel antenna 102 for connecting the transceiver.

[0061] The radome 101 is made of a wave-transmitting composite material, the size of which matches the contour of the flat antenna 102 and has the characteristics of low loss and high strength.

[0062] See also Figure 4 and Figure 7 The GPS receiving module 204 is a GPS / BD dual-mode receiving module. The GPS / BD dual-mode receiving module can automatically switch the positioning system according to the signal strength, thereby improving the applicability of the product.

[0063] In addition, the upper support 100, the middle support 200 and the base 3 are square, and the shapes of the three are adapted to each other. With the square integrated structure, the volume of the device can be integrated smaller, making it more convenient to carry and store.

[0064] The working process of the present invention is as follows: start the power supply, obtain the terminal's location information through the GPS receiving module 204 (GPS / BD dual-mode receiving module), the antenna control unit 201 calculates the heading angle and pitch angle of the flat antenna 102 according to the satellite location information, and then drives the pitch motor 207 and the heading motor 208 to adjust the heading angle and pitch angle of the flat antenna 102 to the angle aligned with the satellite. After the flat antenna 102 is initially aligned with the satellite, the carrier receiver 203 will receive the satellite downlink data signal and demodulate the parameters such as the receiving level and the signal-to-noise ratio. The antenna control unit 201 adjusts the heading angle and pitch angle of the flat antenna 102 within a small range according to the changes in the receiving level and the signal-to-noise ratio to achieve the relative maximum value of the receiving level and the signal-to-noise ratio. During the adjustment process of the pitch angle and the heading angle, the electronic compass 206 and the inclinometer 104 play the role of angle data value feedback, forming a closed-loop control to achieve high-precision adjustment.

[0065] See also Fig.10The satellite communication of the present invention is full-duplex communication for transmission and reception, which is divided into a downlink channel and an uplink channel. After the flat array antenna 102 receives the satellite electromagnetic wave signal, it is frequency-converted, filtered and amplified by the transceiver, and the intermediate frequency signal is transmitted to the digital baseband unit 202 for demodulation and decoding, and finally output through the network port or wifi. After the terminal receives the user IP data, it is encoded and modulated by the digital baseband unit 202 to form an intermediate frequency signal, and the transceiver is used to convert the frequency, filter and amplify it, and finally radiate it toward the satellite through the antenna. Full-duplex communication technology is an existing technical means. The present invention applies the existing full-duplex communication technology and does not improve the full-duplex communication technology. Therefore, the implementation process of this part is not described in detail in this application.

[0066] The communication terminal of the present invention has the following advantages over the prior art:

[0067] 1. It adopts an upper, middle and lower three-layer structure. The flat antenna 102 and the transceiver 103 are installed in the upper support 100, and the signal processing units are installed in the middle support 200. The communication function and the electromechanical control function are integrated. It can be used and stored without installing any accessories, which improves portability and ease of use.

[0068] 2. The flat antenna 102 is used to make the device more regular in shape and smaller in size compared to the traditional parabolic antenna;

[0069] 3. The radio frequency module uses a transceiver 103 with integrated BUC and LNB, which does not require assembly and wiring, and has a shorter opening and closing time, a more compact device, and a smaller use area and storage volume. The layout of each module is designed and integrated, solving the problems of traditional portable satellite communication terminals with many components, large storage volume, and complex operation, making it more convenient to store and carry.

[0070] 4. After powering on, the antenna control unit 201 controls the pitch motor 207 to adjust the angle of the upper support 100 relative to the middle support 200 according to the position information obtained by the GPS receiving module 204, and controls the pitch motor 208 to adjust the rotation angle of the middle support 200 relative to the base 3, thereby automatically adjusting the pitch angle and heading angle and realizing automatic satellite alignment.

[0071] 5. During the antenna attitude (pitch angle and heading angle) adjustment process, the electronic compass 206 and the inclinometer 104 play a role in angle data value feedback, forming a closed-loop control and improving the adjustment accuracy.

[0072] According to the disclosure and teaching of the above description, those skilled in the art to which the present invention belongs may also make changes and modifications to the above embodiments. Therefore, the present invention is not limited to the specific embodiments disclosed and described above, and some modifications and changes to the present invention should also fall within the scope of protection of the claims of the present invention. In addition, although some specific terms are used in this specification, these terms are only for the convenience of description and do not constitute any limitation to the present invention.

Claims

1. A portable integrated satellite communication terminal, comprising: The upper module includes an upper support, and a radome, a flat antenna, a transceiver and an inclinometer mounted thereon, the transceiver integrates a BUC and an LNB, the radome is mounted on the upper side of the upper support, the flat antenna, the transceiver and the inclinometer are mounted in the radome, the transmitting port of the transceiver is connected to the transmitting port of the flat antenna, and the receiving port of the transceiver is connected to the receiving port of the flat antenna; The middle-layer module includes a middle-layer support, and an antenna control unit, a digital baseband unit, a carrier receiver, a GPS receiving module or a GPS / BD dual-mode receiving module, and an electronic compass installed thereon. The rear side of the upper-layer support is connected to the middle-layer support. The intermediate frequency input of the carrier receiver is connected to the intermediate frequency receiving of the transceiver, the intermediate frequency output of the carrier receiver is connected to the intermediate frequency receiving input of the digital baseband, and the intermediate frequency transmitting of the digital baseband is connected to the intermediate frequency transmitting of the transceiver. The antenna control unit is respectively connected to the inclinometer, the carrier receiver, the GPS receiving module, and the electronic compass. A base, rotatably connected to the lower side of the middle support; The pitch motor is installed on the middle support and connected to the antenna control unit. The pitch motor drives the upper support to move relative to the middle support through the pitch transmission assembly to adjust the pitch angle. The heading motor is installed on the middle-level support and connected to the antenna control unit. The pitch motor drives the middle-level support to rotate relative to the base through the heading transmission assembly to adjust the heading angle; The shapes of the radome, the middle support and the base are adapted to each other, the radome is covered on the middle support and the middle support is rotated to be aligned with the base for storage; The radome is provided with an antenna accommodating cavity with an opening at the lower side, the upper support is smaller than the antenna accommodating cavity, the upper support is provided with an upper element chamber with an opening at the upper side, the flat antenna is installed in the antenna accommodating cavity, and the transceiver and the inclinometer are installed in the upper element chamber; The flat panel antenna is a rectangular flat panel array antenna, and the horns arranged vertically and horizontally form the radiation surface of the antenna. The lower surface is provided with a waveguide interface for connecting the transceiver. The transceiver and the inclinometer are installed on the lower side of the flat panel antenna. The middle-level support is provided with a middle-level component room with an upper opening, in which the digital baseband unit, carrier receiver, GPS receiving module, power distribution unit, electronic compass, pitch motor and heading motor are installed; The heading transmission assembly is arranged between the middle support and the base; The middle part of the middle support is rotatably connected to the middle part of the base, and the output end of the heading motor passes through the lower surface of the middle support and is connected to the base through the heading transmission component; The upper support can be placed in the middle component room when stored, and the lower end of the antenna cover peripheral wall matches the upper end of the middle support in shape, so that the lower end of the antenna cover peripheral wall and the upper end of the middle support are spliced ​​together when stored.

2. The portable integrated satellite communication terminal according to claim 1, characterized in that: The pitch motor is installed on the middle support, and the pitch transmission assembly includes a first gear and a second gear, the first gear is connected to the pitch motor, the second gear is fixedly connected to the upper support, and the first gear and the second gear are meshed for transmission; Alternatively, the pitch motor is installed on the upper support, and the pitch transmission assembly includes a first gear and a second gear, the first gear is connected to the pitch motor, the second gear is fixedly connected to the middle support, and the first gear and the second gear are meshed for transmission.

3. The portable integrated satellite communication terminal according to claim 1, characterized in that: The heading transmission assembly includes a third gear and a fourth gear, the third gear is connected to the heading motor, the middle part of the middle support is rotatably connected to the middle part of the base, the fourth gear is coaxially arranged with the rotating axis of the middle support and the base, the fourth gear is fixedly connected to the base, and the third gear and the fourth gear are meshed for transmission.

4. The portable integrated satellite communication terminal according to claim 1, characterized in that: The fourth gear is a toothed disc, a middle portion of which is correspondingly provided with a middle hole, and a middle portion of the middle support is connected with a middle portion of the base through a bearing.

5. The portable integrated satellite communication terminal according to any one of claims 1 to 4, characterized in that: It also includes a power distribution unit, which is connected to an external power source or a built-in battery module. The power distribution unit provides power for each component module on the middle layer module, as well as the pitch motor and the heading motor.

6. The portable integrated satellite communication terminal according to claim 5, characterized in that: The middle support is provided with a rechargeable battery module, and the battery module is electrically connected to the power distribution unit.

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