Titlebook: Design Advances in Aerospace Robotics; Proceedings of TORVE Marco Ceccarelli,Loredana Santo,Giacomo Cupertino Conference proceedings 2023 T

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书目名称Design Advances in Aerospace Robotics影响因子(影响力)




书目名称Design Advances in Aerospace Robotics影响因子(影响力)学科排名




书目名称Design Advances in Aerospace Robotics网络公开度




书目名称Design Advances in Aerospace Robotics网络公开度学科排名




书目名称Design Advances in Aerospace Robotics被引频次




书目名称Design Advances in Aerospace Robotics被引频次学科排名




书目名称Design Advances in Aerospace Robotics年度引用




书目名称Design Advances in Aerospace Robotics年度引用学科排名




书目名称Design Advances in Aerospace Robotics读者反馈




书目名称Design Advances in Aerospace Robotics读者反馈学科排名

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Conference proceedings 2023ots for Space Applications in Orbital Stations (TORVEASTRO), held in Rome, Italy on April 20-21, 2023. Topics addressed include history of space and robotics, bio-inspired space robotics, grasping, handling and intelligent manipulation, kinematics and dynamics, navigation & motion planning, robot vi

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Systems of Uniform Recurrence Equationsrating robots on the International Space Station are underlined. Main criticalities of the Low Earth Orbit environment (radiations, space debris and temperature excursions), as well as those of the launch from the ground to the space station, are described.

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https://doi.org/10.1007/978-1-4614-8420-2nsional design suitable for use in space station service applications. Requirements and characteristics are reviewed to identify design issues and operational characteristics. A feasibility study is outlined using simulations to characterize the fundamental functioning and conduct a performance analysis.

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Scheduling in Parallel Computing Systemssystem architecture and its implementation on the laboratory demonstrator robot, the control design is described. Preliminary control tests of a single arm with its basic movements are then illustrated; finally, the main critical aspects and results are reviewed.

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Vitaly A. Strusevich,Kabir Rustogiic simulation using the Autodesk Inventor package. For defined positions of the satellite and the berthing port, the positions of the end-effector are assumed, and the angular positions of the other joints are measured. The problems of grasping and slipping of the satellite are outlined and solved by changing the geometry of the fingertips.