A satellite simulator for asymmetric pcma

A satellite and load simulation technology, applied in the field of satellite simulation, can solve the problems of difficult test and high cost, and achieve the effect of improving applicability and supporting flexible management of application scenarios

Active Publication Date: 2022-04-12
中国卫通集团股份有限公司
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

Due to the difficulty and high cost of conducting experiments on real satellites, in order to improve the efficiency and quality of distributed HTS communication products developed, a satellite simulator that can truly and stably simulate multi-user hinges on satellites is required

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  • A satellite simulator for asymmetric pcma
  • A satellite simulator for asymmetric pcma

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Embodiment Construction

[0034] In the solutions provided by the embodiments of the present application, the described embodiments are only some of the embodiments of the present application, not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.

[0035] A satellite load simulator for asymmetric PCMA provided by the embodiment of the present application will be described in further detail below in conjunction with the accompanying drawings, see figure 2 , the simulator may specifically include: at least two signal processing circuits 1, at least two signal branching circuits 2, a multi-user hinge relationship simulation module 3 and an interface processing and integrated control module 4; wherein,

[0036] The interface processing and integrated control module 4 is connected to the at least two signal processing circuits 1 fo...

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Abstract

The application discloses a satellite load simulator for asymmetric PCMA, the satellite simulator includes: at least two signal processing circuits, at least two signal branching circuits, multi-user hinge relationship simulation module and interface processing and comprehensive control module; the interface processing and integrated control module is used to adjust the signal processing parameters of each signal processing circuit; each signal processing circuit is used to combine and convert multiple signal beams to obtain digital signals, and process the digital signals according to the signal processing parameters The user hinge relationship simulation module is used to determine the link information of the user, and forwards the processed signal to a signal branching circuit according to the link information; each signal branching circuit is used to receive the processed signal, The processed signal is subjected to frequency conversion conversion processing, and the frequency conversion analog signal is subjected to split processing. This application fills up the technical problem of the satellite simulator blank of the distributed HTS communication system.

Description

technical field [0001] The present application relates to the technical field of satellite simulation, in particular to a satellite load simulator for asymmetric PCMA. Background technique [0002] In the distributed high-throughput satellite (High Throughput Satellite, HTS) communication system, user terminals communicate through outer space satellite transponders. Since the communication process is completely dependent on satellite space resources, but given that the existing space resources on the satellite are insufficient , the paired carrier multiple access (PCMA), which can double the system capacity, is applied to the HTS communication system. Due to the difficulty and high cost of conducting experiments on real satellites, in order to improve the efficiency and quality of distributed HTS communication products developed, a satellite simulator that can truly and stably simulate multi-user hinges on satellites is needed. [0003] see figure 1 , the current process o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B7/185
CPCH04B7/18519
Inventor 田青杨恪王立中陈昱良党金瑞吕韫哲李金亮
Owner 中国卫通集团股份有限公司
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