By Jason Hall
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Extra info for Advances in Spacecraft Technologies
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.
22 au using SEP. The inability of the Solar Orbiter mission to attain a solar polar orbit highlights the difficulty of such a goal with conventional propulsion. It has however been shown that a mid-term solar sail can be used to deliver a spacecraft to a true solar polar orbit in approximately five-years (Goldstein et al, 1998; Macdonald et al, 2006). The Solar Polar Orbiter (SPO) mission concept is a good example of the type of high-energy inner-solar system mission which is enabled by solar sail propulsion.
Hydraulic control systems. ; Wu, X. & Dougal, R. (2005). Interface issues in Hardware-in-the-Loop simulation. Proceedings of the 2005 IEEE Ship Technologies Symposium, Jul. 39-45 Office of Naval Research's Best Manufacturing Practices. (1999). Report of survey conducted at NASA Marshall Space Flight Center. Best Manufacturing Practice Center of Excellence. Huntsville, USA, Apr. 12-13 Peng, C. ; Qu, G. ; Ma, Z. C. & Yu, J. Y. (1992). Russia large spacecraft dynamics and its testing technology. ; Zhao, Y.