scholarly journals Real Sky Tests of Star-Tracker-Based Attitude Determination System for Earth Pointing Spacecraft

2008 ◽  
Vol 56 (657) ◽  
pp. 480-491
Author(s):  
Takanori IWATA ◽  
Eiji HIROKAWA ◽  
Hiroki HOSHINO ◽  
Takeshi YOSHIZAWA ◽  
Koshi SATO ◽  
...  
2016 ◽  
Vol 58 (9) ◽  
pp. 1671-1681 ◽  
Author(s):  
Lijun Zhang ◽  
Shan Qian ◽  
Shifeng Zhang ◽  
Hong Cai

GPS Solutions ◽  
2012 ◽  
Vol 17 (1) ◽  
pp. 129-138 ◽  
Author(s):  
Christian Eling ◽  
Philipp Zeimetz ◽  
Heiner Kuhlmann

Sensors ◽  
2020 ◽  
Vol 20 (24) ◽  
pp. 7296
Author(s):  
Guanqing Li ◽  
Lasse Klingbeil ◽  
Florian Zimmermann ◽  
Shengxiang Huang ◽  
Heiner Kuhlmann

Immersed tunnel elements need to be exactly controlled during their immersion process. Position and attitude of the element should be determined quickly and accurately to navigate the element from the holding area to the final location in the tunnel trench. In this paper, a newly-developed positioning and attitude determination system, integrating a 3-antenna Global Navigation Satellite System (GNSS) system, an inclinometer and a range-measurement system, is presented. The system is designed to provide the absolute position of both ends of the element with sufficient accuracy in real time. Special attention in the accuracy analysis is paid to the influence of GNSS multipath error and sound speed profile. Simulations are conducted to illustrate the performance of the system in different scenarios. If both elements are very close, the accuracies of the system are higher than 0.02 m in the directions perpendicular to and along the tunnel axis.


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