By Jason Hall
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Additional resources for Advances in Spacecraft Technologies
Ph. D. thesis. Harbin, China: Harbin Institute of Technology, Aug. 8-12 (in Chinese) He, J. (2007). Analysis and control of hydraulically driven 6-DOF parallel manipulator. Ph. D. thesis. Harbin, China: Harbin Institute of Technology, Feb. 89-98 (in Chinese) Huang, Q. ; Jiang, H. ; Zhang, S. Y. & Han, J. W. (2005). Spacecraft docking simulation using HIL simulator with Stewart platform. Journal of Chinese Mechanical Engineering. 3, Mar. ; Guan, H. H. (1999). Study on dynamics of mechano-electronic springdamper system with differential connections.
Solar sailing, like other forms of low-thrust propulsion, requires that if a bound orbit about the target body is desired then at arrival the spacecraft must have, in-effect, zero hyperbolic excess velocity. Therefore, any wholly low-thrust interplanetary mission is required, unlike high-thrust missions, to slow-down prior to arrival at the target body and subsequently the transfer duration is typically significantly increased; this is especially true for bodies which can be relatively easily reached by high-thrust, chemical propulsion systems such as Mars and Venus.
2007e). Simulation on HIL ground experimental simulator for on-orbit docking dynamics. Acta Aewnautica et Astwanautica. 4, Jul. 975-980( in Chinese) Chang, T. ; Cong, D. ; Ye, Z. M. & Han, J. W. (2008). Research on fundamental problems and the solutions of HIL simulation for on-orbit docking dynamics. Journal of Astronautics. 1, Jan. 53-55( in Chinese) Chang, T. L. (2010). Research on verification of authenticity of HIL simulation using vibroimpact model. Journal of Vibration and Shock. 1, Jan.