SOLAR SAIL FORCE MODELING FOR SPINNING SOLAR SAIL USING THE RADIOMETRIC TRACKING DATA
SOLAR SAIL FORCE MODELING FOR SPINNING SOLAR SAIL USING THE RADIOMETRIC TRACKING DATA
复制标题
DOI：
10.7446/jaesa.0303.03
复制
发表时间：
2011-09
期刊：
影响因子：
--
通讯作者：
Tomohiro Yamaguchi;H. Ikeda;Y. Mimasu;Y. Tsuda;H. Takeuchi;M. Yoshikawa
中科院分区：
文献类型：
--
作者：
Tomohiro Yamaguchi;H. Ikeda;Y. Mimasu;Y. Tsuda;H. Takeuchi;M. Yoshikawa
摘要：利用辐射跟踪数据研究了IKAROS航天器的太阳帆力模型。太阳帆力模型是实际太阳帆任务的关键参数之一，它直接影响到整个轨道的设计。由于太阳帆的展开及其光学特性，太阳帆力模型可能存在较大的不确定性，因此在发射前对模型进行配置存在困难。本文主要研究了基于发射后信息的旋转型太阳帆力模型的估计。利用几种跟踪条件之间的重叠比较来估计太阳帆加速度。关键词：太阳帆，定轨，导航，航天器建模太阳帆是未来可以扩展深空探测的技术之一，因为太阳帆具有在没有燃料的情况下接收太阳光子动量并获得加速度的能力。许多利用太阳帆进行空间探索的创新应用被研究，例如水星、小行星和外太阳系[1-3]。因此，许多空间组织都在努力实现这一技术。例如，宇宙1号项目由行星学会资助，并试图在地球旋转轨道上展示太阳帆技术（Reichhardt, 2005）。600米
Abstract: This paper investigates the solar sail force modeling of the IKAROS spacecraft using radiometric tracking data. The solar sail force model is one of the key parameter for the practical solar sail mission because the model impacts the overall trajectory design. Since the solar sail force model may have a large uncertainty due to the solar sail deployment and its optical properties, there is a difficulty to configure the model before the launch. This study concentrates on the estimation of solar sail force model for spinning type solar sail with post-launch information. The estimated solar sail acceleration is evaluated with overlap comparison between several tracking conditions. Keywords: Solar sail, Orbit determination, Navigation, Spacecraft modeling. 1 Introduction Solar sail is the one of the future technology could expand the deep space explorations, because solar sail have a capability to receive solar photon momentum and obtain acceleration without fuel. Many innovative applications are investigated using solar sails to for space explorations, for instance Mercury, asteroids and outer solar systems [1-3]. Therefore, many space organizations make efforts to realize the technique. For instance, Cosmos 1 project were funded by Planetary Society and try to demonstrate the solar sail technology on the Earth rotating orbit Reichhardt (2005). The 600 m