DocumentCode :
79559
Title :
Simulation of Multiangular Radar Echoes for Speed Measurement During CE-3 Landing on the Lunar Sinus Iridum Surface
Author :
Hongxia Ye ; Ya-Qiu Jin
Author_Institution :
Key Lab. for Inf. Sci. of Electromagn. Waves, Fudan Univ., Shanghai, China
Volume :
53
Issue :
9
fYear :
2015
fDate :
Sept. 2015
Firstpage :
4922
Lastpage :
4932
Abstract :
The main objective of the Chinese Chang´E-3 (CE-3) lunar satellite is to achieve soft-landing and roving exploration on the lunar surface. A multibeam radar in the lunar lander is implemented to measure the echoes from the lunar rough surface during its descending and to derive the speed of the lander. In this paper, numerical simulation of multiangular radar echoes and speed inversions from Doppler frequency are presented. An area of the Lunar Sinus Iridum bay, as landing site, is specifically selected. The rough surface described with the real DTM data is first divided into triangular patches for numerical Kirchhoff approximation calculation. The radar echoes of multiangular radar beams of CE-3 during the landing are numerically simulated. The echo phase and the Doppler frequency are then derived to obtain the vertical speed.
Keywords :
lunar surface; planetary landers; planetary rovers; CE-3 landing; Chinese Chang´E-3 lunar satellite; Doppler frequency; Kirchhoff approximation calculation; Lunar Sinus Iridum bay; Lunar Sinus Iridum surface; echo phase; landing site; lunar lander; lunar rough surface; multiangular radar echo simulation; multibeam radar; roving exploration; speed measurement; Doppler radar; Moon; Rough surfaces; Scattering; Spaceborne radar; Surface roughness; Chang´E-3 (CE-3); Doppler frequency; multiangular radar; retrieval of range and speed; rough surface scattering; soft-landing;
fLanguage :
English
Journal_Title :
Geoscience and Remote Sensing, IEEE Transactions on
Publisher :
ieee
ISSN :
0196-2892
Type :
jour
DOI :
10.1109/TGRS.2015.2413893
Filename :
7113828
Link To Document :
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