DocumentCode :
1880965
Title :
Innovative astronaut navigation system based on smart integrated sensors
Author :
Benzerrouk, Hamza ; Nebylov, Alexander ; Yatsevitch, Gennady
Author_Institution :
IIAAT, Algeria
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
9
Abstract :
Original algorithms for navigation on the surface of Mars planet, especially applied to astronauts, are proposed in this paper. The autonomous navigation system for astronaut is based on inertial measurement unit (redundant) and Laser (redundant), which permits to localize and navigate in known environment and unknown environment constructing its map in real time, using adaptive algorithms and physical and natural constraints of astronaut´s body. The estimation of the position of astronauts is done using non linear adaptive filters such as the Extended Kalman Filter (EKF) and other non linear variant filters. Finally, additional smart idea is to use Phobos and Deimos as navigation constellation in addition to one more satellite.
Keywords :
Kalman filters; Mars; adaptive filters; navigation; nonlinear filters; planetary satellites; sensors; EKF; Mars planet; adaptive algorithms; extended Kalman Filter; innovative astronaut navigation system; navigation constellation; non linear variant filters; satellite; smart integrated sensors; Earth; Estimation; Gravity; Laser radar; Mars; Satellite navigation systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187112
Filename :
6187112
Link To Document :
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