DocumentCode
2521252
Title
Novel robotic spacecraft simulator with mini-control moment gyroscopes and rotating thrusters
Author
Hall, Jason S. ; Romano, Marcello
Author_Institution
Naval Postgraduate Sch., Monterey
fYear
2007
fDate
4-7 Sept. 2007
Firstpage
1
Lastpage
6
Abstract
A novel hardware-in-the-loop spacecraft simulator is introduced for the laboratory validation of guidance, navigation and control algorithms. This three-degrees-of-freedom robotic vehicle uses the principle of air-floating along a flat floor in order to reproduce in two dimensions the frictionless and weightlessness conditions of the orbital flight. For the first time in its class, to the authors´ knowledge, the new spacecraft simulator uses miniature control moment gyroscopes for the attitude control and rotating thrusters for both attitude and translational control. A pseudo-GPS, a LIDAR and a fiber optic gyroscope are used as navigation sensors. The paper presents in details the design of the robotic vehicle and the results of preliminary experiments.
Keywords
Global Positioning System; aerospace robotics; aerospace simulation; aircraft navigation; attitude control; fibre optic gyroscopes; optical radar; space vehicles; LIDAR; air-floating principle; attitude control; fiber optic gyroscope; miniature control moment gyroscope; navigation sensors; pseudo-GPS; robotic spacecraft simulator; rotating thrusters; three-degrees-of-freedom robotic vehicle; translational control; Attitude control; Gyroscopes; Laser radar; Navigation; Optical fiber sensors; Optical fibers; Optical sensors; Orbital robotics; Robot sensing systems; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Advanced intelligent mechatronics, 2007 IEEE/ASME international conference on
Conference_Location
Zurich
Print_ISBN
978-1-4244-1263-1
Electronic_ISBN
978-1-4244-1264-8
Type
conf
DOI
10.1109/AIM.2007.4412475
Filename
4412475
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