DocumentCode :
1795215
Title :
Positioning reduction of lunar precise landing site based on VLBI tracking data
Author :
Li, J.F. ; Xie, Xiang ; Zhang, Z.B. ; Li, H.N.
Author_Institution :
State Key Lab. of Astronaut. Dynamics, Xi´an, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1877
Lastpage :
1880
Abstract :
In view of the landing site positioning of the lunar probe, this paper proposes a positioning reduction method based on VLBI tracking data, and applies VLBI delay-observation data from more than three baselines to complete positioning reduction with the distance between the lunar lander and the center of the earth as a constraint. Simulation results show that the positioning accuracy of landing point of the lunar lander can reach 100 m if the standard deviation of the VLBI delay-observation noise is less than 1 ns (0.3 m). This method also supports positioning reduction of other deep space probes´ precise landing.
Keywords :
aircraft landing guidance; entry, descent and landing (spacecraft); lunar surface; position control; radiowave interferometry; space research; statistical analysis; VLBI delay-observation data; VLBI delay-observation noise; VLBI tracking data; deep space probes; landing point; landing site positioning; lunar lander; lunar precise landing site; lunar probe; positioning accuracy; positioning reduction method; standard deviation; very long baseline interferometer; Accuracy; Equations; Mathematical model; Moon; Noise; Probes; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007467
Filename :
7007467
Link To Document :
بازگشت