首页> 外文会议>47th international astronautical congress >PASSIVE INTERMODULATION PRODUCTS CONTROL AND VERIFICATION ACTIVITIES IN A MULTICARRIER L-BAND SATELLITE SYSTEM FOR MOBILE COMMUNICATIONS: THE ITALSAT F2/EMS EXPERIENCE
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PASSIVE INTERMODULATION PRODUCTS CONTROL AND VERIFICATION ACTIVITIES IN A MULTICARRIER L-BAND SATELLITE SYSTEM FOR MOBILE COMMUNICATIONS: THE ITALSAT F2/EMS EXPERIENCE

机译:用于移动通信的多载波L波段卫星系统中的无源互调产品控制和验证活动:ITALSAT F2 / EMS经验

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The Italsat F2 satellite has been launched in August 1996: in addition to the domestic mission in Ka-band it embarks the L-band mobile payload (European Mobile System). Passive InterModulation (PIM) products generation is a very critical aspect for L-band payloads working in a multicarrier environment, so the EMS payload was designed to cope with stringent PIM Products requirements, while the spacecraft design, as derived from the first Italsat flight unit, did not focus on PIM aspects. PIM generation is basically caused by currents flowing in components with a non linear voltage-current behaviour, and may occur at equipment, s/s and system level. The EMS payload performance can be affected by the intermodulations generated by two L-band Tx carriers, that could fall in the EMS L-band Rx section; from the EMS frequency plan, the minimum order of these PIM products are the 7th and the 9th. This paper describes the activities carried out from equipment up to satellite level to eliminate as much as possible PIM effects, and the results of the final spacecraft PIM test campaign. The paper is composed by three main parts. The first part deal with the technological aspects of the design and the production of the EMS components considered critical from PIM generation point of view. The second part describes the PIM control strategy applied at spacecraft level, and in the third part the spacecraft PIM test campaign results are presented. cqcr.
机译:Italsat F2卫星已于1996年8月发射:除了在Ka波段进行国内任务外,它还搭载了L波段移动有效载荷(欧洲移动系统)。无源互调(PIM)产品的产生对于在多载波环境中工作的L波段有效载荷至关重要,因此EMS有效载荷旨在满足严格的PIM产品要求,而航天器的设计源自Italsat的首个飞行单元,并未专注于PIM方面。 PIM产生基本上是由电流在非线性电压-电流行为的组件中流动引起的,并且可能发生在设备,s / s和系统级别。 EMS净荷性能可能受到两个L波段Tx载波产生的互调的影响,这可能会落在EMS L波段Rx部分中。从EMS频率计划中,这些PIM产品的最低订购量为第七和第九。本文介绍了从设备到卫星级为消除尽可能多的PIM效应而进行的活动,以及最终的航天器PIM测试活动的结果。本文由三个主要部分组成。第一部分处理从PIM生成角度来看至关重要的EMS组件的设计和生产的技术方面。第二部分描述了应用于航天器级别的PIM控制策略,第三部分介绍了航天器PIM测试活动的结果。 cqcr。

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