Space 2006 2006
DOI: 10.2514/6.2006-7428
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Experimental Demonstration of Technologies for Autonomous On-Orbit Robotic Assembly

Abstract: The Modular Reconfigurable High Energy (MRHE) program aimed to develop technologies for the automated assembly and deployment of large-scale space structures and aggregate spacecraft. Part of the project involved creation of a terrestrial robotic testbed for validation and demonstration of these technologies and for the support of future development activities. This testbed was completed in 2005, and was thereafter used to demonstrate automated rendezvous, docking, and self-assembly tasks between a group of th… Show more

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Cited by 16 publications
(8 citation statements)
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“…At present, many organizations [9][10][11][12] are conducting research on connection technology using space small-scale targets. The autonomous micro-satellite docking system (AMDS) [13,14], developed by the Orbital Express (OE) project, utilized soft-docking technology [15] to buffer the impact.…”
Section: Introductionmentioning
confidence: 99%
“…At present, many organizations [9][10][11][12] are conducting research on connection technology using space small-scale targets. The autonomous micro-satellite docking system (AMDS) [13,14], developed by the Orbital Express (OE) project, utilized soft-docking technology [15] to buffer the impact.…”
Section: Introductionmentioning
confidence: 99%
“…While the MIT Space Laboratory(SSL) has developed the Synchronized Position Hold Engage and Reorient Experimental Satellites (SPHERES) facility for the testing of formation flight in a six degree of freedom(DOF) environment and autonomous docking algorithm and visual navigation inside the ISS, in NASA's reduced gravity aircraft and in a 1-g laboratory environment [8,9], the Lockheed Martin Controls and Automation Laboratory in Palo Alto, California presents a unique environment for the development and testing of technologies associated with automated rendezvous, docking, and self-assembly tasks between a group of modular robotic spacecraft emulators [10]. Moreover, to validation of GN&C methods for the proximity navigation and docking between two small spacecraft of similar mass, the Spacecraft Robotics Laboratory of Naval Postgraduate School is conducting Autonomous Docking and Spacecraft Servicing Simulator (AUDASS) [7,11].…”
Section: Introductionmentioning
confidence: 99%
“…One such method involves reproduction of the kinematics and vehicle dynamics for 3-DoF (two horizontal translational degrees and one rotational degree about the vertical axis) through the use of robotic spacecraft simulators that float via planar air bearings on a flat horizontal floor. This particular method is currently being employed by several research institutions and is the validation method of choice for our research into GNC algorithms for proximity operations at the Naval Postgraduate School (Machida et al, 1992;Ullman, 1993;Corrazzini & How, 1998;Marchesi et al, 2000;Ledebuhr et al, 2001;Nolet et al, 2005;LeMaster et al, 2006;Romano et al, 2007). With respect to spacecraft involved in proximity operations, the in-plane and cross-track dynamics are decoupled, as modeled by the Hill-Clohessy-Wiltshire (HCW) equations, thus the reduction to 3-Degree of Freedom (DoF) does not appear to be a critical limiter.…”
Section: Introductionmentioning
confidence: 99%