CN110865556A - Virtual satellite, virtual satellite-based software and algorithm test platform and method - Google Patents

Virtual satellite, virtual satellite-based software and algorithm test platform and method Download PDF

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CN110865556A
CN110865556A CN201911225870.8A CN201911225870A CN110865556A CN 110865556 A CN110865556 A CN 110865556A CN 201911225870 A CN201911225870 A CN 201911225870A CN 110865556 A CN110865556 A CN 110865556A
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satellite
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CN110865556B (en
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李丹
赵军锁
潘晏涛
张衡
张健
詹乃军
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Abstract

The invention provides a virtual satellite, a test platform and a method based on software and algorithm of the virtual satellite, relating to the technical field of the virtual satellite, wherein the platform comprises: the satellite control and state monitoring tool carries out measurement and control and software/algorithm injection on the virtual satellite and receives the data downloaded by the virtual satellite; the internal testing tool monitors the behavior of the software/algorithm and tests the performance of the software/algorithm; the external test tool performs configuration item testing and/or system testing on the software/algorithm. The virtual satellite decouples the cloud computing platform simulator with the satellite platform simulator and the load simulator by taking the data center as an interface. The invention can improve the integration degree of the simulator through the virtual satellite; the monitoring tool and the testing tool realize efficient sharing and multiplexing of testing resources, and the problem that the existing satellite testing cannot meet multi-region cooperation, distributed execution and large-scale parallel testing is solved.

Description

虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法Virtual satellite, virtual satellite-based software and algorithm test platform and method

技术领域technical field

本发明涉及虚拟卫星技术领域,尤其是涉及一种虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法。The invention relates to the technical field of virtual satellites, in particular to a virtual satellite, a test platform and method for virtual satellite-based software and algorithms.

背景技术Background technique

卫星软件/算法测试的目的是卫星软件/算法使用前对其进行全面有效地检测,得到卫星软件/算法可能存在的问题和设计缺陷,为后续卫星软件/算法的研制提供有利的技术支持,保证软件/算法在卫星上正常运行。The purpose of satellite software/algorithm testing is to comprehensively and effectively test the satellite software/algorithm before it is used, to obtain possible problems and design defects of the satellite software/algorithm, and to provide favorable technical support for the subsequent development of the satellite software/algorithm. The software/algorithms are functioning properly on the satellite.

传统卫星测试中因卫星软硬件紧耦合等原因,无法以纯软件的方式提供一套与在轨卫星相同的软件执行环境,只能依靠物理或半物理仿真的桌面卫星进行测试。模拟器由于运行环境不同、运行方式不同,存在着集成化程度不一致的问题;而且现有技术的桌面卫星造价较高、数量有限,无法满足多地域协同、分布式执行、大规模并行的测试工作。In traditional satellite testing, due to the tight coupling of satellite software and hardware, it is impossible to provide a set of software execution environment that is the same as that of in-orbit satellites in pure software, and can only rely on physical or semi-physical simulated desktop satellites for testing. Due to the different operating environments and operating modes of the simulator, there is a problem of inconsistent degree of integration; and the existing technology of desktop satellites is expensive and limited in number, which cannot meet the multi-regional coordination, distributed execution, and large-scale parallel test work. .

发明内容SUMMARY OF THE INVENTION

有鉴于此,本发明的目的在于提供一种虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法,以提高对模拟器的集成化程度和对测试资源的重复利用率。In view of this, the purpose of the present invention is to provide a virtual satellite, a virtual satellite-based software and algorithm testing platform and method, so as to improve the integration degree of the simulator and the repeated utilization of testing resources.

第一方面,本发明实施例提供了一种虚拟卫星,其中,虚拟卫星包括:卫星平台模拟器、通过数据中心与所述卫星平台模拟器相连的云计算平台模拟器和载荷模拟器,其中,以数据中心作为接口将所述云计算平台模拟器与所述卫星平台模拟器、所述载荷模拟器解除耦合关系;所述卫星平台模拟器,用于仿真卫星平台系统,输出卫星平台数据;所述载荷模拟器,用于仿真有效载荷系统,输出载荷数据;所述云计算平台模拟器,用于提供与在轨卫星相同的基础服务,并读取所述卫星平台数据和所述载荷数据。In a first aspect, an embodiment of the present invention provides a virtual satellite, wherein the virtual satellite includes: a satellite platform simulator, a cloud computing platform simulator and a load simulator connected to the satellite platform simulator through a data center, wherein, The cloud computing platform simulator is decoupled from the satellite platform simulator and the load simulator by using the data center as an interface; the satellite platform simulator is used to simulate the satellite platform system and output satellite platform data; The payload simulator is used to simulate the payload system and output payload data; the cloud computing platform simulator is used to provide the same basic services as the orbiting satellite, and read the satellite platform data and the payload data.

结合第一方面,本发明实施例提供了第一方面的第一种可能的实施方式,其中,云计算平台模拟器包括具有基础服务的Sputnix虚机;Sputnix虚机上装载与在轨卫星相同的基础服务;其中,基础服务包括以下中的至少一种:测控服务、监控管理服务、数传服务、注入服务、平台数据服务和相机服务。In conjunction with the first aspect, the embodiment of the present invention provides the first possible implementation manner of the first aspect, wherein the cloud computing platform simulator includes a Sputnix virtual machine with basic services; the Sputnix virtual machine is loaded with the same foundation as the orbiting satellite. services; wherein, the basic services include at least one of the following: measurement and control services, monitoring and management services, data transmission services, injection services, platform data services, and camera services.

结合第一方面,本发明实施例提供了第一方面的第二种可能的实施方式,其中,所述数据中心包括数据库;所述数据库,用于模拟真实卫星的集成单元部分,获取外部激励的数据。In conjunction with the first aspect, the embodiment of the present invention provides a second possible implementation manner of the first aspect, wherein the data center includes a database; the database is used to simulate the integrated unit part of a real satellite, and obtain external excitation data. data.

结合第一方面,本发明实施例提供了第一方面的第三种可能的实施方式,其中,所述卫星平台模拟器仿真得到的卫星平台系统包括:热控分系统、电源分系统、姿态与轨道控制分系统、推进分系统、测控分系统和数据管理分系统。In conjunction with the first aspect, the embodiment of the present invention provides a third possible implementation manner of the first aspect, wherein the satellite platform system simulated by the satellite platform simulator includes: a thermal control subsystem, a power source subsystem, an attitude and Orbit control subsystem, propulsion subsystem, measurement and control subsystem and data management subsystem.

结合第一方面,本发明实施例提供了第一方面的第四种可能的实施方式,其中,所述载荷模拟器仿真得到的有效载荷系统包括:信息获取分系统、信息传输分系统和信息基准分系统。In conjunction with the first aspect, the embodiment of the present invention provides a fourth possible implementation manner of the first aspect, wherein the payload system simulated by the payload simulator includes: an information acquisition subsystem, an information transmission subsystem, and an information benchmark sub-system.

第二方面,本发明实施例提供一种基于虚拟卫星的软件与算法的测试平台,包括:如第一方面任一可能的实施方式中的虚拟卫星,还包括与所述虚拟卫星中的云计算平台模拟器通信连接的卫星控制与状态监视工具、外部测试工具,以及安装于所述虚拟卫星内部的内部测试工具;所述卫星控制与状态监视工具,用于对所述虚拟卫星进行测控和软件/算法的注入,并接收所述云计算平台模拟器的卫星平台数据和载荷数据;所述内部测试工具,用于对运行于所述虚拟卫星上的所述软件/算法的行为进行监视,并对所述软件/算法进行性能测试;所述外部测试工具,用于对运行于所述虚拟卫星上的所述软件/算法进行配置项测试和/或系统测试。In a second aspect, an embodiment of the present invention provides a test platform for software and algorithms based on virtual satellites, including: a virtual satellite in any possible implementation manner of the first aspect, and a cloud computing system related to the virtual satellite Satellite control and status monitoring tools, external testing tools, and internal testing tools installed inside the virtual satellites that are communicatively connected to the platform simulator; the satellite control and status monitoring tools are used to perform measurement, control and software on the virtual satellites /Injection of the algorithm, and receive the satellite platform data and payload data of the cloud computing platform simulator; the internal testing tool is used to monitor the behavior of the software/algorithm running on the virtual satellite, and Perform performance testing on the software/algorithm; the external testing tool is used to perform configuration item testing and/or system testing on the software/algorithm running on the virtual satellite.

结合第二方面,本发明实施例提供了第二方面的第一种可能的实施方式,其中,内部测试工具包括:行为监视工具和性能测试工具;所述行为监视工具,用于监控所述软件/算法在所述虚拟卫星上运行的过程中的数据流及用户对数据库的操作;所述性能测试工具,用于测试运行于所述虚拟卫星上的所述软件/算法的性能。In conjunction with the second aspect, an embodiment of the present invention provides a first possible implementation manner of the second aspect, wherein the internal testing tool includes: a behavior monitoring tool and a performance testing tool; the behavior monitoring tool is used to monitor the software /Data flow in the process of running the algorithm on the virtual satellite and operations on the database by the user; the performance testing tool is used to test the performance of the software/algorithm running on the virtual satellite.

结合第二方面,本发明实施例提供了第二方面的第二种可能的实施方式,其中,外部测试工具包括:配置项测试工具和/或系统测试工具;所述配置项测试工具,用于对运行于所述虚拟卫星上的所述软件/算法进行配置项测试;所述系统测试工具,用于对运行于所述虚拟卫星上的所述软件/算法进行系统测试。In conjunction with the second aspect, the embodiment of the present invention provides a second possible implementation manner of the second aspect, wherein the external testing tool includes: a configuration item testing tool and/or a system testing tool; the configuration item testing tool is used for The configuration item test is performed on the software/algorithm running on the virtual satellite; the system testing tool is used to perform a system test on the software/algorithm running on the virtual satellite.

结合第二方面的第二种可能的实施方式,本发明实施例提供了第三方面的第一种可能的实施方式,其中,所述外部测试工具以及所述卫星控制与状态监视工具均通过TCP/IP协议与所述云计算平台模拟器进行信息交换。In conjunction with the second possible implementation manner of the second aspect, the embodiment of the present invention provides the first possible implementation manner of the third aspect, wherein the external testing tool and the satellite control and status monitoring tool all use TCP The /IP protocol exchanges information with the cloud computing platform simulator.

第三方面,本发明实施例提供一种基于虚拟卫星的软件与算法的测试方法,其中,所述方法应用于如第二方面任一项所述的测试平台,所述方法包括:初始化虚拟卫星,所述虚拟卫星包括云计算平台模拟器、卫星平台模拟器和载荷模拟器,所述云计算平台模拟器通过数据中心分别与所述卫星平台模拟器、载荷模拟器解除耦合关系;通过卫星控制与状态监视工具,对所述虚拟卫星进行测控和软件/算法的注入,并接收所述云计算平台模拟器的卫星平台数据和载荷数据;通过内部测试工具对运行于所述虚拟卫星上的所述软件/算法的行为进行监视,并对所述软件/算法进行性能测试;通过外部测试工具对运行于所述虚拟卫星上的所述软件/算法进行配置项测试和/或系统测试。In a third aspect, an embodiment of the present invention provides a method for testing software and algorithms based on virtual satellites, wherein the method is applied to the test platform according to any one of the second aspects, and the method includes: initializing the virtual satellite , the virtual satellite includes a cloud computing platform simulator, a satellite platform simulator and a load simulator, and the cloud computing platform simulator is decoupled from the satellite platform simulator and the load simulator through the data center respectively; With the status monitoring tool, the virtual satellite is monitored and controlled and the software/algorithm is injected, and the satellite platform data and load data of the cloud computing platform simulator are received; monitor the behavior of the software/algorithm, and perform performance testing on the software/algorithm; perform configuration item testing and/or system testing on the software/algorithm running on the virtual satellite through an external testing tool.

本发明实施例带来了以下有益效果:The embodiments of the present invention have brought the following beneficial effects:

本发明提供的一种虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法,该平台包括:卫星控制与状态监视工具,用于对虚拟卫星进行测控和软件/算法的注入,并接收云计算平台模拟器的卫星平台数据和载荷数据;内部测试工具,用于对运行于虚拟卫星上的软件/算法的行为进行监视,并对软件/算法进行性能测试;外部测试工具,用于对运行于虚拟卫星上的软件/算法进行配置项测试和/或系统测试。该虚拟卫星包括:卫星平台模拟器,用于仿真卫星平台系统,输出卫星平台数据;载荷模拟器,用于仿真有效载荷系统,输出载荷数据;云计算平台模拟器,用于提供与在轨卫星相同的基础服务,并读取卫星平台数据和载荷数据;其中,以数据中心作为接口将云计算平台模拟器与卫星平台模拟器、载荷模拟器解耦。本发明通过云计算平台模拟器中的数据中心,将云计算模拟器与卫星平台模拟器、载荷模拟器进行解耦,将云计算平台之外的部分作为构件集成到虚拟卫星中,可以提高模拟器的集成化程度;通过监视工具及测试工具,可以实现高效共享及复用测试资源,从而缓解现有卫星测试中存在的无法满足多地域协同、分布式执行、大规模并行测试的问题。The present invention provides a virtual satellite, a virtual satellite-based software and algorithm testing platform and method. The platform includes satellite control and state monitoring tools, which are used for monitoring and controlling virtual satellites and injecting software/algorithms, and receiving cloud Satellite platform data and payload data of the computing platform simulator; internal test tools for monitoring the behavior of software/algorithms running on virtual satellites and performance testing of software/algorithms; external test tools for running Perform configuration item testing and/or system testing on software/algorithms on virtual satellites. The virtual satellite includes: a satellite platform simulator for simulating a satellite platform system and outputting satellite platform data; a payload simulator for simulating a payload system and outputting payload data; a cloud computing platform simulator for providing communication with on-orbit satellites The same basic service, and read satellite platform data and load data; among them, the data center is used as an interface to decouple the cloud computing platform simulator from the satellite platform simulator and the load simulator. The invention decouples the cloud computing simulator from the satellite platform simulator and the load simulator through the data center in the cloud computing platform simulator, and integrates the parts other than the cloud computing platform into the virtual satellite as components, which can improve the simulation The integration degree of the device; through monitoring tools and testing tools, efficient sharing and reuse of test resources can be achieved, thereby alleviating the problems existing in existing satellite testing that cannot meet multi-regional coordination, distributed execution, and large-scale parallel testing.

本发明的其他特征和优点将在随后的说明书中阐述,并且,部分地从说明书中变得显而易见,或者通过实施本发明而了解。本发明的目的和其他优点在说明书、权利要求书以及附图中所特别指出的结构来实现和获得。Other features and advantages of the present invention will be set forth in the description which follows, and in part will be apparent from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the description, claims and drawings.

为使本发明的上述目的、特征和优点能更明显易懂,下文特举较佳实施例,并配合所附附图,作详细说明如下。In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, preferred embodiments are given below, and are described in detail as follows in conjunction with the accompanying drawings.

附图说明Description of drawings

为了更清楚地说明本发明具体实施方式或现有技术中的技术方案,下面将对具体实施方式或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本发明的一些实施方式,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to illustrate the specific embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the specific embodiments or the prior art. Obviously, the accompanying drawings in the following description The drawings are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings without creative efforts.

图1为本发明实施例提供的虚拟卫星的结构示意图;1 is a schematic structural diagram of a virtual satellite provided by an embodiment of the present invention;

图2为本发明实施例提供的卫星平台模拟器的结构示意图;2 is a schematic structural diagram of a satellite platform simulator provided by an embodiment of the present invention;

图3为本发明实施例提供的虚拟卫星另一种结构示意图;3 is another schematic structural diagram of a virtual satellite provided by an embodiment of the present invention;

图4为本发明实施例提供的一种测试平台的结构示意图;4 is a schematic structural diagram of a test platform provided by an embodiment of the present invention;

图5为本发明实施例提供的基于虚拟卫星的软件与算法的测试方法流程图。FIG. 5 is a flowchart of a method for testing software and algorithms based on virtual satellites provided by an embodiment of the present invention.

具体实施方式Detailed ways

为使本发明实施例的目的、技术方案和优点更加清楚,下面将结合附图对本发明的技术方案进行清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the present invention, but not all of them. example. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

目前,传统卫星测试中因卫星软硬件紧耦合等原因,无法以纯软件的方式提供一套与在轨卫星相同的软件执行环境,只能依靠物理或半物理仿真的桌面卫星进行测试,模拟器由于运行环境不同、运行方式不同,存在着集成化程度不一致的问题。虚拟卫星是一套全新理念的卫星资源整合系统,用户通过虚拟卫星定购数据时,无需考虑卫星本身的类型,只是向该系统提供卫星配置要求,虚拟卫星就可以将目前所有的卫星资源进行整合,向用户提供标准化数据产品以及全面的解决方案。基于此,本发明实施例提供的虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法,可以使得虚拟卫星程序执行环境与在轨卫星完全兼容,且配有众多的后台仿真程序和载荷模拟器,为应用程序提供了一个和真实卫星一致的运行视图。虚拟卫星测试环境可按需加载运行,满足多地域协同、分布式执行、大规模并行的测试需求,可以解决现有技术的桌面卫星中存在的造价较高、数量有限,无法满足多地域协同、分布式执行、大规模并行的测试工作的问题。At present, due to the tight coupling of satellite software and hardware in traditional satellite testing, it is impossible to provide a set of software execution environment that is the same as that of in-orbit satellites in pure software. The operating environment is different, the operating mode is different, and there is a problem of inconsistency in the degree of integration. Virtual satellite is a new concept of satellite resource integration system. When users order data through virtual satellite, they do not need to consider the type of satellite itself, but only provide satellite configuration requirements to the system, and virtual satellite can integrate all current satellite resources. Provide users with standardized data products and comprehensive solutions. Based on this, the virtual satellite, the virtual satellite-based software and algorithm test platform and method provided by the embodiments of the present invention can make the virtual satellite program execution environment fully compatible with the orbiting satellite, and are equipped with numerous background simulation programs and load simulation programs. , which provides the application with a consistent view of the operation of a real satellite. The virtual satellite test environment can be loaded and run on demand to meet the multi-regional collaboration, distributed execution, and large-scale parallel testing requirements. The problem of distributed execution, massively parallel test work.

为便于对本实施例进行理解,首先对本发明实施例所公开的一种虚拟卫星进行详细介绍。To facilitate understanding of this embodiment, a virtual satellite disclosed in the embodiment of the present invention is first introduced in detail.

实施例一:Example 1:

本实施例提供一种虚拟卫星,其结构示意图如图1所示,包括:卫星平台模拟器120、通过数据中心140与卫星平台模拟器120相连的云计算平台模拟器110和载荷模拟器130,其中,以数据中心140作为接口将云计算平台模拟器110与卫星平台模拟器120、载荷模拟器130解除耦合关系。This embodiment provides a virtual satellite, the schematic diagram of which is shown in FIG. 1 , including: a satellite platform simulator 120 , a cloud computing platform simulator 110 and a load simulator 130 connected to the satellite platform simulator 120 through a data center 140 , The cloud computing platform simulator 110 is decoupled from the satellite platform simulator 120 and the load simulator 130 by using the data center 140 as an interface.

云计算平台模拟器110,用于提供与在轨卫星相同的基础服务,并读取卫星平台数据和载荷数据;The cloud computing platform simulator 110 is used to provide the same basic services as the orbiting satellites, and to read satellite platform data and payload data;

卫星平台模拟器120,用于仿真卫星平台系统,输出卫星平台数据;The satellite platform simulator 120 is used to simulate the satellite platform system and output the satellite platform data;

载荷模拟器130,用于仿真有效载荷系统,输出载荷数据。The payload simulator 130 is used to simulate the payload system and output payload data.

具体的,云计算平台模拟器110通过数据中心140,分别与卫星平台模拟器120和载荷模拟器130进行数据和指令的交互。在实际应用中,数据中心140可以包括数据库,用于模拟真实卫星的集成单元部分,直接接收或读取外部激励的数据。通过数据中心140使得卫星平台模拟器120、载荷模拟器130与云计算平台模拟器110的耦合关系得到解除,从而实现将云计算平台之外的部分作为构件集成到虚拟卫星中,以及解决由于模拟器运行环境不同、运行方式不同而导致的集成化程度不一致的问题。Specifically, the cloud computing platform simulator 110 exchanges data and instructions with the satellite platform simulator 120 and the payload simulator 130 through the data center 140, respectively. In practical applications, the data center 140 may include a database for simulating the integrated unit part of a real satellite, directly receiving or reading externally stimulated data. Through the data center 140, the coupling relationship between the satellite platform simulator 120, the load simulator 130 and the cloud computing platform simulator 110 is released, so as to realize the integration of parts other than the cloud computing platform into the virtual satellite as components, and to solve the problems caused by simulation The problem of inconsistency in the degree of integration caused by different operating environments and different operating modes of the server.

卫星平台模拟器120和载荷模拟器130均可根据一定的配置参数仿真出具有不同能力的卫星平台系统和有效荷载,从而为不同类型的软件定义卫星服务。这些模拟器的设计采用类插件的模式,使用数据库定义模拟器接口,将模拟器作为插件组件,可独立定制,即插即用,极大地提高了模拟卫星中模拟器的应用便捷性。Both the satellite platform simulator 120 and the payload simulator 130 can simulate satellite platform systems and payloads with different capabilities according to certain configuration parameters, so as to define satellite services for different types of software. The design of these simulators adopts the plug-in-like model, uses the database to define the simulator interface, and uses the simulator as a plug-in component, which can be independently customized and plug-and-play, which greatly improves the application convenience of the simulator in the simulated satellite.

在实际应用中,卫星平台主要有热控制、电源、姿态与轨道控制、测控、数据管理等功能。相应的,卫星平台有各自对应的模拟器,如图2所示,模拟器中包含卫星平台模拟器120和载荷模拟器130;其中,卫星平台模拟器120仿真得到的卫星平台系统诸如包括:热控分系统、电源分系统、姿态与轨道控制分系统、推进分系统、测控分系统和数据管理分系统;载荷模拟器130仿真得到的有效载荷系统诸如包括:信息获取分系统、信息传输分系统和信息基准分系统。In practical applications, the satellite platform mainly has functions such as thermal control, power supply, attitude and orbit control, measurement and control, and data management. Correspondingly, the satellite platforms have their corresponding simulators. As shown in FIG. 2 , the simulators include a satellite platform simulator 120 and a load simulator 130; wherein, the satellite platform system simulated by the satellite platform simulator 120 includes, for example: Control subsystem, power source subsystem, attitude and orbit control subsystem, propulsion subsystem, measurement and control subsystem, and data management subsystem; the payload system simulated by the load simulator 130 includes, for example, information acquisition subsystem, information transmission subsystem and Information Benchmarking System.

在一些实现方式中,参照图3所示的虚拟卫星另一种结构示意图,云计算平台模拟器110可以是一台基于Sputnix系统以提供一定基础服务的Sputnix虚机,通过Sputnix虚机可以解除卫星软硬件之间的耦合关系,这使得云计算平台模拟器110可以脱离卫星硬件的限制,提供与在轨飞行的软件定义卫星完全兼容的执行环境。Sputnix虚机中装载了与在轨卫星相同的基础服务,诸如包括测控服务、监控管理服务、数传服务、注入服务、平台数据服务和相机服务等。In some implementations, referring to another schematic structural diagram of the virtual satellite shown in FIG. 3 , the cloud computing platform simulator 110 may be a Sputnix virtual machine based on the Sputnix system to provide certain basic services, and the satellite can be deactivated through the Sputnix virtual machine. The coupling relationship between software and hardware enables the cloud computing platform simulator 110 to break away from the limitations of satellite hardware and provide an execution environment that is fully compatible with software-defined satellites flying in orbit. The Sputnix virtual machine is loaded with the same basic services as in-orbit satellites, such as measurement and control services, monitoring management services, data transmission services, injection services, platform data services, and camera services.

考虑到被测软件及算法的测试过程与数据转发链路不相关,本实施例可以使用数据中心140(在本实施例中该数据中心140为数据库)模拟真实卫星的采集单元部分,并由数据库直接接收或读取预设的测控数传模拟器150、成像载荷模拟器131、卫星平台模拟器120等外部激励的数据。Considering that the testing process of the software under test and the algorithm is not related to the data forwarding link, this embodiment can use the data center 140 (in this embodiment, the data center 140 is the database) to simulate the acquisition unit part of the real satellite, and use the database to simulate the acquisition unit part of the real satellite. Directly receive or read the preset measurement and control data transmission simulator 150 , imaging load simulator 131 , satellite platform simulator 120 and other externally stimulated data.

诸如,成像载荷模拟器131可以通过相机服务将成像载荷数据发送至数据库;卫星平台模拟器120可以通过平台数据服务将卫星平台数据发送至数据库;数据库可以通过数传服务将数传数据传递至测控数传模拟器150;而测控数传模拟器150可以通过测控服务将测控指令传递至数据库;数据库还可以通过软件/算法、监控管理服务和注入服务等与卫星平台模拟器120、云计算平台模拟器110和载荷模拟器130进行数据指令的交互。For example, the imaging payload simulator 131 can send the imaging payload data to the database through the camera service; the satellite platform simulator 120 can send the satellite platform data to the database through the platform data service; the database can transmit the data transmission data to the measurement and control through the data transmission service The data transmission simulator 150; the measurement and control data transmission simulator 150 can transmit the measurement and control instructions to the database through the measurement and control service; the database can also simulate the satellite platform simulator 120 and the cloud computing platform through software/algorithms, monitoring management services and injection services, etc. The controller 110 and the payload simulator 130 interact with data commands.

本实施例通过数据中心140使得卫星平台模拟器120、成像载荷模拟器131与云计算平台模拟器110的耦合关系得到解除,实现了将云计算平台之外的部分作为构件集成到虚拟卫星中,解决了由于模拟器运行环境不同、运行方式不同而导致的集成化程度不一致的问题。In this embodiment, the coupling relationship between the satellite platform simulator 120, the imaging load simulator 131 and the cloud computing platform simulator 110 is released through the data center 140, so that the parts other than the cloud computing platform are integrated into the virtual satellite as components, Solved the problem of inconsistency in the degree of integration caused by different simulator operating environments and operating modes.

实施例二:Embodiment 2:

基于上述实施例所提供的虚拟卫星,本实施例提供了一种基于虚拟卫星的软件与算法的测试平台,如图4所示,该测试平台包括上述实施例中的虚拟卫星,还包括与虚拟卫星中的云计算平台模拟器110通信连接的卫星控制与状态监视工具210、外部测试工具,以及安装于虚拟卫星内部的内部测试工具。Based on the virtual satellites provided by the above embodiments, this embodiment provides a test platform for software and algorithms based on virtual satellites. As shown in FIG. 4 , the test platform includes the virtual satellites in the above embodiments, and also includes a virtual satellite based The cloud computing platform simulator 110 in the satellite is communicatively connected to the satellite control and status monitoring tool 210, the external test tool, and the internal test tool installed inside the virtual satellite.

虚拟卫星,其实现原理及产生的技术效果和前述实施一中提到的虚拟卫星相同,在此不再详细阐述。The realization principle and the technical effect of the virtual satellite are the same as those of the virtual satellite mentioned in the foregoing implementation 1, and will not be described in detail here.

卫星控制与状态监视工具210,用于对虚拟卫星进行测控和软件/算法的注入,并接收云计算平台模拟器110的卫星平台数据和载荷数据。The satellite control and status monitoring tool 210 is used to perform measurement and control and software/algorithm injection for virtual satellites, and receive satellite platform data and payload data from the cloud computing platform simulator 110 .

具体的,卫星控制与状态监视工具210对虚拟卫星的测控诸如对卫星姿态的监测与控制、对轨道的监测与控制、对星上时间的监测与控制和遥控遥测等。卫星控制与状态监视工具210可以通过注入服务将软件/算法注入至虚拟卫星,以使软件/算法在虚拟卫星上运行。卫星控制与状态监视工具210还可以接收云计算平台模拟器110下传的卫星平台数据和载荷数据。Specifically, the satellite control and state monitoring tool 210 monitors and controls virtual satellites, such as monitoring and control of satellite attitude, orbit monitoring and control, on-board time monitoring and control, and remote telemetry. The satellite control and condition monitoring tool 210 may inject software/algorithms into the virtual satellite through an injection service, so that the software/algorithm runs on the virtual satellite. The satellite control and status monitoring tool 210 can also receive satellite platform data and payload data downloaded by the cloud computing platform simulator 110 .

内部测试工具,用于对运行于虚拟卫星上的软件/算法的行为进行监视,并对软件/算法进行性能测试。Internal testing tools are used to monitor the behavior of software/algorithms running on virtual satellites and perform performance testing of software/algorithms.

外部测试工具,用于对运行于虚拟卫星上的软件/算法进行配置项测试和/或系统测试。External testing tools for configuration item testing and/or system testing of software/algorithms running on virtual satellites.

在一些实施方式中,内部测试工具包括行为监视工具232和性能测试工具231。行为监视工具232,用于监控软件/算法在虚拟卫星上运行的过程中的数据流及用户对数据库的操作;性能测试工具231,用于测试运行于虚拟卫星上的软件/算法的性能。In some embodiments, internal testing tools include behavior monitoring tools 232 and performance testing tools 231 . The behavior monitoring tool 232 is used to monitor the data flow of the software/algorithm running on the virtual satellite and the user's operation on the database; the performance testing tool 231 is used to test the performance of the software/algorithm running on the virtual satellite.

在一些实施方式中,外部测试工具包括:配置项测试工具221和/或系统测试工具222。配置项测试工具221,用于通过虚拟卫星外部系统对运行于虚拟卫星上的软件/算法进行配置项测试;系统测试工具222,用于通过虚拟卫星外部系统对运行于虚拟卫星上的软件/算法进行系统测试。In some embodiments, the external testing tools include: configuration item testing tools 221 and/or system testing tools 222 . The configuration item testing tool 221 is used to test the configuration item of the software/algorithm running on the virtual satellite through the external system of the virtual satellite; the system testing tool 222 is used to test the software/algorithm running on the virtual satellite through the external system of the virtual satellite Perform system tests.

上述的配置项测试工具221、系统测试工具222、卫星控制与状态监视工具210均可以通过TCP/IP(Transmission Control Protocol/Internet Protocol,传输控制协议/因特网互联协议)协议与虚拟卫星中的云计算平台模拟器110进行信息交换。The above-mentioned configuration item testing tool 221, system testing tool 222, satellite control and state monitoring tool 210 can all pass through TCP/IP (Transmission Control Protocol/Internet Protocol, Transmission Control Protocol/Internet Protocol) protocol and cloud computing in the virtual satellite. The platform simulator 110 exchanges information.

本实施例通过虚拟卫星提供了一套与在轨卫星完全兼容的卫星软件/算法执行环境,从而构建一套基于虚拟卫星的软件与算法的测试平台,可实现对卫星软件/算法测试资源进行高效的共享及复用,满足多卫星软件/算法地域协同、分布式执行、大规模并行的卫星软件/算法测试需求。This embodiment provides a set of satellite software/algorithm execution environments that are fully compatible with on-orbit satellites through virtual satellites, thereby constructing a set of virtual satellite-based software and algorithm testing platforms, which can realize efficient testing of satellite software/algorithm testing resources. The sharing and multiplexing of multi-satellite software/algorithms meet the needs of satellite software/algorithm testing for multi-satellite software/algorithm regional collaboration, distributed execution, and large-scale parallelism.

上述实施例中,通过数据中心接口可以使得真实卫星和虚拟卫星同样的既能够接入真正的运行环境,也可以接入虚拟测试环境,因此提供了更真实的测试环境。当虚拟卫星数据注入到数据中心时,可以做虚拟卫星和软件/算法的测试;当真实卫星接入到数据中心时,可以直接对真实卫星进行测控。In the above embodiment, the real satellite and the virtual satellite can be connected to both the real operating environment and the virtual test environment through the data center interface, thus providing a more realistic test environment. When the virtual satellite data is injected into the data center, the virtual satellite and software/algorithm can be tested; when the real satellite is connected to the data center, the real satellite can be directly measured and controlled.

实施例三:Embodiment three:

基于上述实施例所提供的虚拟卫星和基于虚拟卫星的软件与算法的测试平台,本发明实施例提供了一种基于虚拟卫星的软件与算法的测试方法,参见图5所示,该方法包括以下步骤:Based on the virtual satellite and the virtual satellite-based software and algorithm test platform provided by the above embodiments, the embodiment of the present invention provides a virtual satellite-based software and algorithm testing method, as shown in FIG. 5 , the method includes the following step:

步骤S510,初始化虚拟卫星,虚拟卫星包括云计算平台模拟器、卫星平台模拟器和载荷模拟器,云计算平台模拟器通过数据中心分别与卫星平台模拟器、载荷模拟器解除耦合关系;Step S510, initialize the virtual satellite, the virtual satellite includes a cloud computing platform simulator, a satellite platform simulator and a load simulator, and the cloud computing platform simulator is decoupled from the satellite platform simulator and the load simulator through the data center respectively;

步骤S520,通过卫星控制与状态监视工具,对虚拟卫星进行测控和软件/算法的注入,并接收云计算平台模拟器的卫星平台数据和载荷数据;Step S520, perform measurement and control and software/algorithm injection on the virtual satellite through satellite control and state monitoring tools, and receive satellite platform data and load data of the cloud computing platform simulator;

步骤S530,通过内部测试工具对运行于虚拟卫星上的软件/算法的行为进行监视,并对软件/算法进行性能测试;Step S530, monitoring the behavior of the software/algorithm running on the virtual satellite through an internal test tool, and performing performance testing on the software/algorithm;

步骤S540,通过外部测试工具对运行于虚拟卫星上的软件/算法进行配置项测试和/或系统测试。Step S540, perform configuration item test and/or system test on the software/algorithm running on the virtual satellite by using an external test tool.

上述方法通过数据中心,可以实现将云计算平台之外的部分作为构件集成到虚拟卫星中,从而解决由于模拟器运行环境不同、运行方式不同而导致的集成化程度不一致的问题;而且上述方法中的测试工具通过虚拟卫星,提供了一套与在轨卫星完全兼容的卫星软件/算法执行环境,从而构建一套基于虚拟卫星的软件与算法云测试平台,可实现对卫星软件/算法测试资源进行高效的共享及复用,满足多卫星软件/算法地域协同、分布式执行、大规模并行的卫星软件/算法测试需求。The above method can realize the integration of the parts other than the cloud computing platform as components into the virtual satellite through the data center, so as to solve the problem of inconsistency in the degree of integration caused by different operating environments and operating modes of the simulator; The test tool provides a set of satellite software/algorithm execution environment that is fully compatible with in-orbit satellites through virtual satellites, thereby building a set of virtual satellite-based software and algorithm cloud test platforms, which can realize the satellite software/algorithm test resources. Efficient sharing and multiplexing to meet the multi-satellite software/algorithm regional collaboration, distributed execution, and massive parallel satellite software/algorithm testing requirements.

本发明实施例所提供的方法,其实现原理及产生的技术效果和前述实施例一和二中的实施例相同,为简要描述,方法实施例部分未提及之处,可参考前述方法实施例中相应内容。The implementation principles and technical effects of the methods provided in the embodiments of the present invention are the same as those in the foregoing embodiments 1 and 2. For the sake of brief description, for the parts not mentioned in the method embodiments, reference may be made to the foregoing method embodiments. corresponding content.

综上,上述发明实施例提供的虚拟卫星、基于虚拟卫星的软件与算法的测试平台及方法,该平台包括:卫星控制与状态监视工具,用于对虚拟卫星进行测控和软件/算法的注入,并接收云计算平台模拟器的卫星平台数据和载荷数据;内部测试工具,用于对运行于虚拟卫星上的软件/算法的行为进行监视,并对软件/算法进行性能测试;外部测试工具,用于对运行于虚拟卫星上的软件/算法进行配置项测试和/或系统测试。该虚拟卫星包括:卫星平台模拟器,用于仿真卫星平台系统,输出卫星平台数据;载荷模拟器,用于仿真有效载荷系统,输出载荷数据;云计算平台模拟器,用于提供与在轨卫星相同的基础服务,并读取卫星平台数据和载荷数据;其中,以数据中心作为接口将云计算平台模拟器与卫星平台模拟器、载荷模拟器解耦。本发明通过云计算平台模拟器中的数据中心,将云计算模拟器与卫星平台模拟器、载荷模拟器进行解耦,将云计算平台之外的部分作为构件集成到虚拟卫星中,可以提高模拟器的集成化程度;通过监视工具及测试工具,可以实现高效共享及复用测试资源,从而缓解现有卫星测试中存在的无法满足多地域协同、分布式执行、大规模并行测试的问题。To sum up, the virtual satellite, virtual satellite-based software and algorithm test platform and method provided by the above-mentioned embodiments of the invention, the platform includes: satellite control and status monitoring tools, used for monitoring and controlling the virtual satellite and injecting software/algorithms, And receive the satellite platform data and payload data of the cloud computing platform simulator; internal testing tools, used to monitor the behavior of software/algorithms running on virtual satellites, and perform performance testing of software/algorithms; external testing tools, used For configuration item testing and/or system testing of software/algorithms running on virtual satellites. The virtual satellite includes: a satellite platform simulator for simulating a satellite platform system and outputting satellite platform data; a payload simulator for simulating a payload system and outputting payload data; a cloud computing platform simulator for providing communication with on-orbit satellites The same basic service, and read satellite platform data and load data; among them, the data center is used as an interface to decouple the cloud computing platform simulator from the satellite platform simulator and the load simulator. The invention decouples the cloud computing simulator from the satellite platform simulator and the load simulator through the data center in the cloud computing platform simulator, and integrates the parts other than the cloud computing platform into the virtual satellite as components, which can improve the simulation The integration degree of the device; through monitoring tools and testing tools, efficient sharing and reuse of test resources can be achieved, thereby alleviating the problems existing in existing satellite testing that cannot meet multi-regional coordination, distributed execution, and large-scale parallel testing.

所属领域的技术人员可以清楚地了解到,为描述的方便和简洁,上述描述的系统、装置和单元的具体工作过程,可以参考前述方法实施例中的对应过程,在此不再赘述。Those skilled in the art can clearly understand that, for the convenience and brevity of description, the specific working process of the above-described systems, devices and units may refer to the corresponding processes in the foregoing method embodiments, which will not be repeated here.

作为分离部件说明的单元可以是或者也可以不是物理上分开的,作为单元显示的部件可以是或者也可以不是物理单元,即可以位于一个地方,或者也可以分布到多个网络单元上。可以根据实际的需要选择其中的部分或者全部单元来实现本实施例方案的目的。Units described as separate components may or may not be physically separated, and components shown as units may or may not be physical units, that is, may be located in one place, or may be distributed to multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution in this embodiment.

另外,在本发明各个实施例中的各功能单元可以集成在一个处理单元中,也可以是各个单元单独物理存在,也可以两个或两个以上单元集成在一个单元中。In addition, each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically alone, or two or more units may be integrated into one unit.

功能如果以软件功能单元的形式实现并作为独立的产品销售或使用时,可以存储在一个处理器可执行的非易失的计算机可读取存储介质中。基于这样的理解,本发明的技术方案本质上或者说对现有技术做出贡献的部分或者该技术方案的部分可以以软件产品的形式体现出来,该计算机软件产品存储在一个存储介质中,包括若干指令用以使得一台计算机设备(可以是个人计算机,服务器,或者网络设备等)执行本发明各个实施例方法的全部或部分步骤。而前述的存储介质包括:U盘、移动硬盘、只读存储器(ROM,Read-OnlyMemory)、随机存取存储器(RAM,Random Access Memory)、磁碟或者光盘等各种可以存储程序代码的介质。The functions, if implemented in the form of software functional units and sold or used as stand-alone products, may be stored in a processor-executable non-volatile computer-readable storage medium. Based on this understanding, the technical solution of the present invention can be embodied in the form of a software product in essence, or the part that contributes to the prior art or the part of the technical solution. The computer software product is stored in a storage medium, including Several instructions are used to cause a computer device (which may be a personal computer, a server, or a network device, etc.) to execute all or part of the steps of the methods of various embodiments of the present invention. The aforementioned storage medium includes: U disk, removable hard disk, Read-Only Memory (ROM, Read-Only Memory), Random Access Memory (RAM, Random Access Memory), magnetic disk or optical disk and other media that can store program codes.

最后应说明的是:以上所述实施例,仅为本发明的具体实施方式,用以说明本发明的技术方案,而非对其限制,本发明的保护范围并不局限于此,尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,其依然可以对前述实施例所记载的技术方案进行修改或可轻易想到变化,或者对其中部分技术特征进行等同替换;而这些修改、变化或者替换,并不使相应技术方案的本质脱离本发明实施例技术方案的精神和范围,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应所述以权利要求的保护范围为准。Finally, it should be noted that the above-mentioned embodiments are only specific implementations of the present invention, and are used to illustrate the technical solutions of the present invention, but not to limit them. The protection scope of the present invention is not limited thereto, although referring to the foregoing The embodiment has been described in detail the present invention, those of ordinary skill in the art should understand: any person skilled in the art who is familiar with the technical field within the technical scope disclosed by the present invention can still modify the technical solutions described in the foregoing embodiments. Or can easily think of changes, or equivalently replace some of the technical features; and these modifications, changes or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention, and should be covered in the present invention. within the scope of protection. Therefore, the protection scope of the present invention should be based on the protection scope of the claims.

Claims (10)

1. A virtual satellite, comprising: the system comprises a satellite platform simulator, a cloud computing platform simulator and a load simulator, wherein the cloud computing platform simulator is connected with the satellite platform simulator through a data center, and the cloud computing platform simulator, the satellite platform simulator and the load simulator are decoupled by taking the data center as an interface;
the satellite platform simulator is used for simulating a satellite platform system and outputting satellite platform data;
the load simulator is used for simulating an effective load system and outputting load data;
the cloud computing platform simulator is used for providing basic services the same as those of an orbiting satellite and reading the satellite platform data and the load data.
2. The virtual satellite of claim 1, wherein the cloud computing platform simulator comprises a Sputnix virtual machine with a base service; loading the basic service same as that of the on-orbit satellite on the Sputnix virtual machine;
wherein the base service comprises at least one of: measurement and control service, monitoring management service, data transmission service, injection service, platform data service and camera service.
3. The virtual satellite of claim 1, wherein the data center comprises a database;
the database is used for simulating an integrated unit part of a real satellite and acquiring data of external excitation.
4. The virtual satellite of claim 1, wherein the satellite platform system simulated by the satellite platform simulator comprises: the system comprises a thermal control subsystem, a power supply subsystem, an attitude and track control subsystem, a propulsion subsystem, a measurement and control subsystem and a data management subsystem.
5. The virtual satellite of claim 1, wherein the payload system simulated by the load simulator comprises: the system comprises an information acquisition subsystem, an information transmission subsystem and an information reference subsystem.
6. A virtual satellite-based software and algorithm test platform, comprising the virtual satellite according to any one of claims 1 to 5, further comprising a satellite control and status monitoring tool communicatively connected to a cloud computing platform simulator in the virtual satellite, an external test tool, and an internal test tool installed inside the virtual satellite;
the satellite control and state monitoring tool is used for carrying out measurement and control and software/algorithm injection on the virtual satellite and receiving satellite platform data and load data of the cloud computing platform simulator;
the internal testing tool is used for monitoring the behavior of the software/algorithm running on the virtual satellite and testing the performance of the software/algorithm;
the external testing tool is used for carrying out configuration item testing and/or system testing on the software/algorithm running on the virtual satellite.
7. The test platform of claim 6, wherein the internal test tool comprises: a behavior monitoring tool and a performance testing tool;
the behavior monitoring tool is used for monitoring data flow of the software/algorithm in the process of running on the virtual satellite and the operation of a user on a database;
the performance testing tool is used for testing the performance of the software/algorithm running on the virtual satellite.
8. The test platform of claim 6, wherein the external test tool comprises: configuring an item test tool and/or a system test tool;
the configuration item testing tool is used for carrying out configuration item testing on the software/algorithm running on the virtual satellite;
the system testing tool is used for carrying out system testing on the software/algorithm running on the virtual satellite.
9. The test platform of claim 8, wherein the external test tool and the satellite control and status monitoring tool each exchange information with the cloud computing platform simulator via a TCP/IP protocol.
10. A virtual satellite based software and algorithm testing method, applied to the test platform according to any one of claims 6-9, the method comprising:
initializing a virtual satellite, wherein the virtual satellite comprises a cloud computing platform simulator, a satellite platform simulator and a load simulator, and the cloud computing platform simulator is respectively decoupled from the satellite platform simulator and the load simulator through a data center;
measuring and controlling the virtual satellite and injecting software/algorithm through a satellite control and state monitoring tool, and receiving satellite platform data and load data of the cloud computing platform simulator;
monitoring the behavior of the software/algorithm running on the virtual satellite through an internal test tool, and performing performance test on the software/algorithm;
performing configuration item testing and/or system testing on the software/algorithms running on the virtual satellite through an external testing tool.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111679906A (en) * 2020-05-11 2020-09-18 长沙天仪空间科技研究院有限公司 Satellite platform capable of uniformly distributing top-level resources and multiplexing and load multiplexing method
CN112083661A (en) * 2020-08-04 2020-12-15 上海航天控制技术研究所 Integrated virtual simulation test system
CN112304653A (en) * 2020-09-07 2021-02-02 航天科工空间工程发展有限公司 Universal comprehensive test method and system for satellite test
CN115220367A (en) * 2022-09-21 2022-10-21 北京航天驭星科技有限公司 Virtual satellite measurement and control simulation method and device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102354123A (en) * 2011-07-18 2012-02-15 北京航空航天大学 Cross-platform extendible satellite dynamic simulation test system
CN106342316B (en) * 2011-07-29 2014-08-13 中国航天科技集团公司第五研究院第五一三研究所 Aeronautical satellite platform high-fidelity satellite simulation general framework system
US20160020848A1 (en) * 2014-07-15 2016-01-21 Digitalglobe, Inc. Integrated architecture for near-real-time satellite imaging applications
CN109660291A (en) * 2019-01-08 2019-04-19 上海卫星工程研究所 A kind of general hardware architecture of load reuse satellite
CN110501722A (en) * 2019-08-14 2019-11-26 上海卫星工程研究所 The satellite in orbit simulation system and method for software definition

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102354123A (en) * 2011-07-18 2012-02-15 北京航空航天大学 Cross-platform extendible satellite dynamic simulation test system
CN106342316B (en) * 2011-07-29 2014-08-13 中国航天科技集团公司第五研究院第五一三研究所 Aeronautical satellite platform high-fidelity satellite simulation general framework system
US20160020848A1 (en) * 2014-07-15 2016-01-21 Digitalglobe, Inc. Integrated architecture for near-real-time satellite imaging applications
CN109660291A (en) * 2019-01-08 2019-04-19 上海卫星工程研究所 A kind of general hardware architecture of load reuse satellite
CN110501722A (en) * 2019-08-14 2019-11-26 上海卫星工程研究所 The satellite in orbit simulation system and method for software definition

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
崔伟光等: "卫星分系统仿真测试平台设计与实现", 《计算机测量与控制》 *
赵军锁等: "发展软件定义卫星的总体思路与技术实践", 《卫星与网络》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111679906A (en) * 2020-05-11 2020-09-18 长沙天仪空间科技研究院有限公司 Satellite platform capable of uniformly distributing top-level resources and multiplexing and load multiplexing method
CN111679906B (en) * 2020-05-11 2023-07-18 长沙天仪空间科技研究院有限公司 Satellite platform for uniformly distributing and multiplexing top-layer resources and load multiplexing method
CN112083661A (en) * 2020-08-04 2020-12-15 上海航天控制技术研究所 Integrated virtual simulation test system
CN112304653A (en) * 2020-09-07 2021-02-02 航天科工空间工程发展有限公司 Universal comprehensive test method and system for satellite test
CN115220367A (en) * 2022-09-21 2022-10-21 北京航天驭星科技有限公司 Virtual satellite measurement and control simulation method and device
CN115220367B (en) * 2022-09-21 2022-12-27 北京航天驭星科技有限公司 Virtual satellite measurement and control simulation method and device

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