Real-time orbit determination onboard SFU (Space Flyer Unit) using GPS data

机译：使用GPS数据实时确定SFU（太空飞行器）的轨道

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The Space flyer unit (SFU) is an unmanned, retrievable and reusable multi-purpose space platform. It was launched by the jananese H-II launch vehicle in March 1995 and was retrieved by the United State's Space shuttle STS-72. We tried real-time orbit determination for the SFU using Global Positioning System (GPS), and the expeirment was very successful. In addition to the free-flight, we were able to evaluate continuous real-time OD solution during orbital manewuvers and attitude control. The real-time orgbit solutions from the experimental GPS receiver onboard the SFU are evaluated in view of their accuracy and reliability for use in SFU orbit determination.

机译：太空飞行器单元（SFU）是无人驾驶，可回收和可重复使用的多功能太空平台。它是由Jananese的H-II运载火箭于1995年3月发射的，并被美国的航天飞机STS-72取回。我们尝试使用全球定位系统（GPS）对SFU进行实时轨道确定，这一实验非常成功。除了自由飞行，我们还能够评估在轨道机动和姿态控制期间的连续实时OD解决方案。考虑到SFU轨道确定中使用的准确性和可靠性，对来自SFU机载实验GPS接收机的实时orgbit解决方案进行了评估。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.307-310|共4页
会议地点 Seoul(KR)
作者
K.Ninomiya; T.Nishimura; M.Mitsutake; H.Kuroda;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
Space Flyer Unit (SFU); Global Positioning System (GPS); Onboard GPS Receiver; Real-time orgbit Determination; Autonomous Navigation;

机译：太空飞行器单元（SFU）；全球定位系统（GPS）；车载GPS接收器；实时orgbit确定自主导航;

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机译：基于RINEX / DORIS 3.0相位数据和星载GPS数据的低地球轨道卫星实时轨道确定
2. Precise Onboard Real-Time Orbit Determination with a Low-Cost Single-Frequency GPS/BDS Receiver [J] . Xuewen Gong, Lei Guo, Fuhong Wang, Remote Sensing . 2019,第11期

机译：低成本单频GPS / BDS接收机进行精确的机载实时轨道确定
3. GPS-based onboard real-time orbit determination for leo satellites using consider Kalman filter [J] . Yang Yang, Xiaokui Yue, Andrew G. Dempster IEEE Transactions on Aerospace and Electronic Systems . 2016,第2期

机译：考虑卡尔曼滤波器的基于GPS的狮子座星载实时轨道确定
4. Real-time orbit determination onboard SFU (Space Flyer Unit) using GPS data [C] . K.Ninomiya, T.Nishimura, M.Mitsutake, International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：使用GPS数据实时轨道确定SFU（空间传单单元）
5. Error assessment of an autonomous real-time precision orbit determination program for a low-earth-orbit satellite using GPS observation data. [D] . Jo, Jung Hyun. 2002

机译：使用GPS观测数据的低地球轨道卫星自主实时精度轨道确定程序的误差评估。
6. Centimeter-Level Orbit Determination for TG02 Spacelab Using Onboard GNSS Data [O] . Kai Li, Xuhua Zhou, Wenbin Wang, 2018

机译：利用机载GNSS数据确定TG02太空实验室的厘米级轨道
7. A Novel Method for Precise Onboard Real-Time Orbit Determination with a Standalone GPS Receiver [O] . Fuhong Wang, Xuewen Gong, Jizhang Sang, 2015

机译：一种用独立Gps接收机精确测量板载实时定轨的新方法
8. Ground data system for Space Flyer Unit (SFU) [R] . Yamada, Takahiro, Sasaki, Susumu, Ninomiya, Keiken 1993

机译：空间飞行器单元（sFU）的地面数据系统

Real-time orbit determination onboard SFU (Space Flyer Unit) using GPS data

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