DocumentCode :
381619
Title :
SPHERES: Development of an ISS Laboratory for formation flight and docking research
Author :
Otero, Alvar Saenz ; Chen, Allen ; Miller, David W. ; Hilstad, Mark
Author_Institution :
Space Syst. Lab., MIT, Cambridge, MA, USA
Volume :
1
fYear :
2002
fDate :
2002
Firstpage :
21551
Abstract :
The MIT Space Systems Laboratory (SSL) is developing the SPHERES (Synchronized Position Hold Engage Reorient Experimental Satellites) formation flight testbed to provide multiple investigators with a long term, replenishable, and upgradable testbed for the validation of high risk metrology, control, and autonomy technologies. These technologies are critical to the operation of distributed satellite and docking missions such as TechSat21, Starlight, Terrestrial Planet Finder, and Orbital Express. The development of SPHERES follows the guidelines set in a laboratory design philosophy created from lessons learned through the development and operation of prior microgravity testbeds by the MIT SSL. The philosophy ensures that the resulting laboratory provides a risk-tolerant and cost-effective environment that facilitates the design process and reduces the development costs of unproven technologies. The testbed consists of three free flyer units which can control their relative positions and orientations in six degrees of freedom. The testbed can operate in 2D on a laboratory platform and in 3D on NASA´s KC-135 and inside the International Space Station. Flight tests aboard NASA´s KC-135 and studies in the ground laboratory confirm the functionality of SPHERES.
Keywords :
aerospace test facilities; artificial satellites; space research; space vehicles; zero gravity experiments; 3D testbed operation; International Space Station; MIT Space Systems Laboratory; NASA KC-135; Orbital Express; SPHERES ISS laboratory; SPHERES formation flight testbed; Starlight; TechSat21; Terrestrial Planet Finder; autonomy technologies; control technologies; design process; development costs; distributed satellite missions; docking; docking missions; flight tests; formation flight; free flyer units; ground laboratory; laboratory design philosophy; laboratory platform 2D operation; metrology technologies; microgravity testbeds; risk-tolerant cost-effective environment; upgradable testbed; Control systems; Guidelines; Laboratories; Metrology; Planetary orbits; Planets; Process design; Satellites; Space technology; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1036828
Filename :
1036828
Link To Document :
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