An overview of formation flying technology development for the Terrestrial Planet Finder mission

M. Aung, A. Ahmed, M. Wette, D. Scharf, J. Tien, G. Purcell, M. Regehr, B. Landin
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引用次数: 28

Abstract

The objective of the Terrestrial Planet Finder (TPF) mission is to find and characterize earth-like planets orbiting other stars. Three architectural options are under consideration for this mission: a formation-flying interferometer (FFI), a structurally-connected interferometer, and a coronagraph. One of these options can be selected as the TPF baseline design in 2006. This paper describes the technology tasks underway to establish the viability of precision formation flying for the FFI option. In particular, interferometric science observations require autonomous precise control and maneuvering of five spacecraft to an accuracy of 2 cm in range and 1 arc-minute in bearing. This precision must be maintained over interspacecraft ranges varying from a few meters to hundreds of meters. Autonomous operations, ranging from formation acquisition and formation maneuvering to high precision formation flying during science observations, are required. Challenges lie in meeting the demanding performance requirements as well as in demonstrating the long-term robustness of the autonomous formation flying system. These challenges are unprecedented for deep space missions. To address them, research is under way in the areas of formation control algorithms, relative sensor technologies, system design, end-to-end real-time system simulation, and ground-based and micro-g end-to-end system demonstrations. Four interrelated testbeds are under development concurrently with the FFI system design. The testbeds include the formation algorithms & simulation testbed (FAST), the formation sensor testbed (FST), the formation control testbed (FCT) and the synchronized position hold engage re-orient experimental satellites (SPHERES) experiment. Formation flying technologies developed under the StarLight project and the NASA Distributed Spacecraft Technology (DST) program are being leveraged and expanded to meet the TPF requirements. This paper provides an overview of the ongoing precision formation flying technology development activities.
类地行星探测任务编队飞行技术发展概况
类地行星发现者(TPF)任务的目标是发现和描述围绕其他恒星运行的类地行星。该任务正在考虑三种结构方案:编队飞行干涉仪(FFI)、结构连接干涉仪和日冕仪。这些方案之一可以被选为2006年的TPF基线设计。本文描述了为确定FFI方案的精确编队飞行可行性而进行的技术任务。特别是,干涉科学观测需要5个航天器的自主精确控制和机动,其距离精度为2厘米,方位精度为1弧分。这种精度必须在航天器间几米到几百米的范围内保持。自主操作,从编队获取和编队机动到科学观测期间的高精度编队飞行,都是必需的。挑战在于满足苛刻的性能要求以及证明自主编队飞行系统的长期鲁棒性。这些挑战对于深空任务来说是前所未有的。为了解决这些问题,研究人员正在进行地层控制算法、相关传感器技术、系统设计、端到端实时系统仿真以及地面和微端到端系统演示等领域的研究。四个相互关联的试验台正在与FFI系统设计同时开发。实验平台包括编队算法与仿真实验平台(FAST)、编队传感器实验平台(FST)、编队控制实验平台(FCT)和同步定位对接实验卫星(SPHERES)实验平台。在星光项目和NASA分布式航天器技术(DST)项目下开发的编队飞行技术正在被利用和扩展,以满足TPF的要求。本文综述了当前精密编队飞行技术的发展现状。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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