2006
DOI: 10.1117/12.665348
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Contact dynamics simulations for robotic servicing of Hubble Space Telescope

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“…Dq + Hq + fq = J p F p (22) where J p denotes the motion Jacobian matrix associated with contact points. The pose trajectory of the container is predicted from the initial conditions and equation (22). If the docking frame is always in the docking domain of the docking hook, then it is determined that the docking is successful.…”
Section: ) Robotic Arm-container Combined Body Contact Dynamics Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…Dq + Hq + fq = J p F p (22) where J p denotes the motion Jacobian matrix associated with contact points. The pose trajectory of the container is predicted from the initial conditions and equation (22). If the docking frame is always in the docking domain of the docking hook, then it is determined that the docking is successful.…”
Section: ) Robotic Arm-container Combined Body Contact Dynamics Modelmentioning
confidence: 99%
“…Aiming at an SRMS end-effector, Akira Tsuchihashi completed the design of a torque sensor and a positioning sensor based on a micro-stroke switch, and proposed a terminal effector docking operation strategy [20]. Jiegao Wang conducted a contact dynamics simulation of an SRMS end-effector for a robotic arm docking operation used in the maintenance of the Hubble space telescope and a derailment service robot system, and proposed an on-orbit autonomous docking strategy for a robotic system [21], [22]. Yisong Tan developed a set of devices made up of a large robotic arm end-effector for the space station, and proposed the docking strategy of a loop/contact transport module [23].…”
Section: Introductionmentioning
confidence: 99%