Titlebook: Aerospace Robotics II; Jerzy Sąsiadek Book 2015 Springer International Publishing Switzerland 2015 Aerospace Robotics.CARO.Conference on A

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书目名称Aerospace Robotics II影响因子(影响力)学科排名




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书目名称Aerospace Robotics II网络公开度学科排名




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书目名称Aerospace Robotics II被引频次学科排名




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书目名称Aerospace Robotics II年度引用学科排名




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书目名称Aerospace Robotics II读者反馈学科排名

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,Innovative Resistojet Propulsion System—Use in Robotic Space Platforms,The high demands of precision and reliability make the simplicity of any such system one of its most important features. In many missions, electrothermal propulsion is considered to be a good solution, but high power levels are required to improve the working gas parameters. Resistojet, designed and

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Analyses of a Free-Floating Manipulator Control Scheme Based on the Fixed-Base Jacobian with Spacecite must be taken into account. Various methods were proposed for control of such systems. In this study we focus on the Jacobian-based Cartesian control and analyze the control scheme based on the fixed-base Jacobian inverse with addition of satellite velocity feedback (i.e., feedback from measurem

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,TwinCube—Preliminary Study of a Tether Experiment for CubeSat Mission,rm two-point diagnostic measurements of electromagnetic emissions in near-Earth plasma. Multi-point measurements play a significant role in understanding energy flows driven by Sun as well as terrestrial activity. Since CubeSats are expected to be low-cost and robust, development of a small and effi

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Novel Type of Inertial Actuator for Satellite Attitude Control System Basis on Concept of Reaction Systems used in spacecrafts, traditionally consists of one to four reaction wheels (RW) or control moment gyroscopes (CMG). In a principle, the attitude of the satellite can be changed by the reaction to the acceleration of the appropriate wheel. In practice, for optimization, redundancy purposes a

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Deployable Manipulator Technology with Application for UAVs,se (UAV or satellite). Low mass is, therefore, a key requirement for manipulator design. Few technology demonstrators for space manipulators have been developed so far. Aerial manipulators are also being researched in terms of potential future applications (e.g., emergency management). In this paper

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,MERTIS/BEPI COLOMBO Pointing Unit Mechanism—Pointing Accuracy Test Procedure, Setup and Results,ents of Mercury’s surface temperatures in the spectral range of 7–14 μm.MERTIS Pointing Unit (MPOI) is a mechanism situated in front of MERTIS spectrometer to orient the optical entrance of the instrument to 4 different targets sequentially. MPOI should fulfill very demanding requirements of pointin