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首页> 外文期刊>Journal of Spacecraft and Rockets >Real-Time Navigation for Mars Missions Using the Mars Network
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Real-Time Navigation for Mars Missions Using the Mars Network

机译:使用火星网络实时导航火星任务

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A NASA Mars technology program task is developing a prototype, embedded, real-time navigation system for Mars final approach and entry, descent, and landing using the Mars Network's Electra ultrahigh frequency transceiver. The Mars Network is ideally situated to provide spacecraft-to-spacecraft navigation via the Electra ultrahigh frequency transceiver, which is a versatile telecommunications payload that is capable of providing autonomous on-orbit, real-time trajectory determination using two-way Doppler measurements between a Mars approach vehicle and a Mars Network orbiter. A set of analyses based on the 2010 encounter at Mars between the Mars Science Laboratory and the Mars Reconnaissance Orbiter demonstrate that the navigation system is capable of achieving a 300 m or better atmosphere entry knowledge error and that the resulting technology is a key component to enabling pinpoint landing. The development approach, software design, and test results from an engineering development unit are presented.
机译:NASA火星技术计划的任务是使用火星网络的Electra超高频收发器为火星的最终进近和下降,着陆开发原型,嵌入式实时导航系统。火星网络的理想位置是通过Electra超高频收发器提供航天器到航天器的导航,Electra超高频收发器是一种通用的电信有效载荷,能够通过使用两点之间的多普勒测量来提供自主的在轨实时轨迹确定火星进近飞行器和火星网络轨道器。根据2010年火星科学实验室与火星侦察轨道飞行器之间在火星上的相遇进行的一组分析表明,导航系统能够实现300 m或更佳的大气进入知识误差,而由此产生的技术是实现这一目标的关键要素精确着陆。介绍了工程开发部门的开发方法,软件设计和测试结果。

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