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Micro (Cost) Technologies for Spacecraft Control Command : an Example, Balloon-Borne Stabilised Gondolas

机译:Spacecraft Control&Commanct的Micro(成本)技术:一个例子,气球传播稳定的长平底球

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Balloons are long-time known space vehicles for science missions and technology in-flight experiments, with instruments that need out-of-atmosphere or in-situ measurements, thus being complementary to the satellite. They carry micro (few hundred grams) to mega (few tons) payloads, but all of them require micro cost, short development, multiple flights. Among the big ones, CNES stabilised gondolas are versatile space platforms used to fly science instruments mainly coming for aeronomy and astrophysics communities, and requiring stabilisation and pointing capabilities, analogous to satellite attitude control subsystems. For them, cost and development constraints cannot be met without highly flexible architectures and off-the-shelf components. In order to increase gondola flexibility to new missions (or adaptability to mission evolutions), new hardware and software solution have been studied for control & command, including stabilisation and pointing functions. Promoted technologies are those of industrial computers, ground networks, free software and, over all, Ada language, for they are open, standard, powerful, low-cost and long-lasting solutions. After a brief description of domain-oriented characteristics of the stabilised gondola control & command, this paper introduces the various technologies and main design principles proposed to meet system-level goals. Then focus is put on on-board architectures : full Ada95 real-time distributed applications on an Ethernet-IP LAN of industrial PCs running Linux, and describes the prototyping work and preliminary development done to ensure feasibility. The paper then discusses the applicability of such solutions to global, ground-to-board, distributed control & command applications, through an IP-based telemetry & telecommand link, such as the one under development in CNES for balloon systems. As a conclusion, this paper shows how adoption of these technologies for other space programs such as satellite platforms and payloads may change design, development costs, duration and organisation, as well as it may open new ways in ground-to-board communication and spacecraft operation.
机译:气球是长期以来的知名空间车辆,用于科学任务和技术在飞行中实验,具有需要外氛围或原位测量的仪器,从而与卫星互补。他们携带微观(几百克)到Mega(几吨)有效载荷,但所有这些都需要微观成本,开发短,多次航班。在大型之中,CNES稳定的缆车是多功能的空间平台,用于飞行主要用于航空和天体物理社区的科学仪器,并要求稳定和指向能力,类似于卫星姿态控制子系统。对于它们,没有高度灵活的架构和现成的组件,不能满足成本和开发限制。为了提高缆车对新任务的灵活性(或对任务演变的适应性),已经研究了新的硬件和软件解决方案,用于控制和命令,包括稳定和指向功能。促销的技术是工业计算机,地面网络,自由软件以及超过所有,ADA语言的技术,因为它们是开放的,标准,强大,低成本和持久的解决方案。在稳定的缆车控制和指挥的面向领域的特征简要说明之后,本文介绍了各种技术和主要设计原则,提出符合系统级目标。然后将焦点放在板载架构:完整的ADA95在运行Linux的工业PCS的Ethernet-IP LAN上的完整ADA95实时分布式应用程序,并描述了对确保可行性的原型工作和初步开发。然后,本文通过基于IP的遥测和电信链接讨论了这种解决方案对全球,地板,分布式控制和指挥应用程序的适用性,例如在CNES用于气球系统中的开发中的开发。作为结论,本文显示了如何为其他空间计划采用这些技术,如卫星平台和有效载荷,可能会改变设计,开发成本,持续时间和组织,以及它可能在地板通信和航天器中开辟新的方式手术。

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