By Jason Hall

ISBN-10: 9533075511

ISBN-13: 9789533075518

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3, Mar. ; Guan, H. H. (1999). Study on dynamics of mechano-electronic springdamper system with differential connections. J. Tsinghua Univ. (Sci. 8, Aug. ; Uchiyama, M. (2001). Analytical and experimental evaluation of impact dynamics on a high-speed zero G motion simulator. Proceedings of the 2001 IEEE/RSJ International Conference on Intelligent Robots and Systems. Hawaii, USA, Oct. 39~45. ; Piedboeuf, J. ; Kovecses, J. (2002). Towards Docking Emulation Using Hardware in the Loop Simulation with Parallel Platform.

Shows the relationship between the reference frame of the motion simulator and the reference frame of spacecrafts bodies. It shows the transform from the position and pose signal of the spacecraft bodies of real-time simulation model to the command signal of the motion simulator. In engineering, the two force and torque sensor scheme of the HIL simulation system bring some difficult in system tuning. When the mass of moving part of the active docking mechanism is relatively small, the force and torque sensor can be calculated out with signals from the force and torque sensor fixed on the rack by Equation (12) and Equation (13).

Time problems in HIL simulation for on-orbit docking and compensation. 841-846. IEEE Industrial Electronics (IE) Chapter & Harbin Institute of Technology, Ma. 2007, Harbin, China, Chang, T. ; Cong, D. ; Ye, Z. M. & Han, J. W. (2007c). Electro-hydraulic servo control system design of HIL simulator for spacecraft on-orbit docking. Proceedings of the Fifth International Symposium on Fluid Power Transmission and Control (ISFP2007), Yansan University, Beidaihe, China, Jul. 2007: 580~584. Chang, T. ; Cong, D.

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Advances in Spacecraft Technologies by Jason Hall

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