DocumentCode :
691180
Title :
Relative Navigation and Guidance Technologies for Rendezvous and Docking
Author :
An Kai ; Tang Zhaoting
Author_Institution :
Shandong Aerosp. Electro-Technol. Inst., Yantai, China
fYear :
2013
fDate :
21-23 Sept. 2013
Firstpage :
1228
Lastpage :
1232
Abstract :
Relative navigation and guidance is a key operational technology required for rendezvous and docking. This paper intends to describe and review some recent patents related to the methods and devices of relative navigation and guidance, including laser guidance, GNSS and UWB guidance, and relative navigation using laser range finder. Corresponding to each of these patents, some reformative approaches and methods are presented in the paper. Especially, a method based on Hill equation is presented which can produce a state estimate to replace the interrupted the visible sensor measurement when, for example, the target satellite is in shadow and the Sun´s rays do not illuminate the target.
Keywords :
Global Positioning System; aircraft landing guidance; artificial satellites; laser ranging; photodetectors; state estimation; ultra wideband technology; GNSS; Hill equation; UWB guidance; docking; laser guidance; laser range finder; photodetector; reformative approach; relative navigation; rendezvous; state estimation; visible sensor measurement; Distance measurement; Global Positioning System; Measurement by laser beam; Semiconductor lasers; Space vehicles; Relative navigation; relative position; relative velocity; rendezvous and docking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2013 Third International Conference on
Conference_Location :
Shenyang
Type :
conf
DOI :
10.1109/IMCCC.2013.273
Filename :
6840663
Link To Document :
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