首页> 外文会议>58th International Astronautical Congress 2007 >A MULTI-PURPOSE AND FULLY AUTONOMOUS IN-FLIGHT MONITORING SYSTEM FOR LAUNCHERS
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A MULTI-PURPOSE AND FULLY AUTONOMOUS IN-FLIGHT MONITORING SYSTEM FOR LAUNCHERS

机译:用于发射器的多用途,全自动飞行监控系统

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Based on the success of several Ariane 5 missions (test satellites, on-board video system etc.) Kayser-Threde has developed a flexible concept for a multipurpose In-Flight Monitoring System (FMS) for launchers due to the fact, that during launcher qualification and for so-called technological flights (post-qualification) a significant higher number of measurement data has to be monitored and transmitted to ground than during nominal operation flights. Even during operational flights there might be the need to have more in-flight monitoring data than the nominal launcher on-board system is able to acquire and to transmit to ground. This multi-purpose Flight Monitoring System includes an Environmental Measurement System (EMS) in combination with an Online Camera system (OCAM) and an Electro-Pyrotechnic Order capability (EPO) offering a complete FMS system for in-flight monitoring. The system consists of a complete infrastructure with own power subsystem, data acquisition and signal conditioning subsystem and telemetry unit. This additional unit can be placed wherever respective envelope is available, typically in the payload bay or on the upper stage.
机译:基于Ariane 5几次任务(测试卫星,机载视频系统等)的成功,Kayser-Threde开发了一种灵活的概念,适用于发射器的多功能机上监控系统(FMS),原因是在发射器期间资格认证和所谓的技术飞行(资格认证后),与正常运行飞行相比,必须监视并大量传输到地面的测量数据。即使在正常飞行期间,可能也需要比标称发射器机载系统能够获取和传输到地面的更多的飞行中监视数据。该多功能飞行监控系统包括一个环境测量系统(EMS),一个在线摄像头系统(OCAM)和一个电子烟火订购功能(EPO),可为飞行中的监控提供完整的FMS系统。该系统由具有自己的电源子系统,数据采集和信号调节子系统以及遥测单元的完整基础架构组成。该附加单元可以放置在有可用信封的任何地方,通常在有效载荷托架中或上层平台中。

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