[1] JEWISON C M. Reconfigurable Thruster Selection Algorithms for Aggregative Spacecraft Systems ［D］. Cambridge: Massachusetts Institute of Technology, 2014.

[2] LIU SH T, HU R, ZHOU P, et al.. Topologic optimization for configuration design of web-skin-type ground structure based large-aperture space mirror ［J］. Opt. Precision Eng, 2013, 21(7): 1803-1810.(in Chinese)

[3] JIN G, ZHANG L, HU F SH. Investigation on space optical system of high F number and high resolution ［J］. Opt. Precision Eng, 2007, 15(2): 155-159.(in Chinese)

[4] ZHOU CH. Research on Modeling and Simulation Analysis for Large Telescope System ［D］. Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2011.(in Chinese)

[5] GARDNER J P, MATHER J C, CLAMPIN M, et al.. The james webb space telescope ［J］. Space Science Reviews, 2006, 123(4): 485-606.

[6] MILLER D, SAENZ-OTERO A, WERTZ J, et al.. SPHERES: a testbed for long duration satellite formation flying in micro-gravity conditions ［C］. Proceedings of the AAS/AIAA space flight mechanics meeting. Clearwater, Florida, January, 2000: 167-179.

[7] MOHAN S, SAKAMOTO H, MILLER D W. Formation control and reconfiguration through synthetic imaging formation flying testbed (SIFFT) ［C］. UV/Optical/IR Space Telescopes: Innovative Technologies and Concepts Ⅲ. International Society for Optics and Photonics, 2007: 66871E-66871E-11.

[8] MACHAIRAS K, ANDREOU S, PARASKEVAS I, et al. Extending the NTUA space robot emulator for validating complex on-orbit servicing tasks ［C］. 12th Symposium on Advanced Space Technologies in Robotics and Automation (ASTRA), 2013.

[9] UNDERWOOD C, PELLEGRINO S, LAPPAS V J, et al.. Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope (AAReST) ［J］. Acta Astronautica, 2015, 114: 112-122.

[10] LIU J, GAO Q, LIU Z, et al.. Attitude control for astronautassisted robot in the space station ［J］. International Journal of Control Automation & Systems, 2016, 14(4): 1082-1095.

[11] GAO Q, LIU J, TIAN T, et al.. Free-flying dynamics and control of an astronaut assistant robot based on fuzzy sliding mode algorithm ［J］. Acta Astronautica, 2017, 138: 462-474.

[12] SCHWARTZ J L, PECK M A, HALL C D. Historical eeview of air-bearing spacecraft simulators ［J］. Journal of Guidance Control & Dynamics, 2003, 26(4): 513-522.

[13] HE J P, XU ZH B, YU Y, et al.. Design and experimental testing of a 9-DOF hyper-redundant robotic arm ［J］. Opt. Precision Eng, 2017, 25(12): 80-86.(in Chinese)

[14] ZHU ZH X. YUAN J P. SHANG P, et al.. Construction of Microgravity Environment for Spacecraft Operation ［M］. Beijing: China Aerospace publishing house, 2013: 23-154.(in Chinese)

[15] XU J. Prototype Development and Research on Key Technologies of the Five Degrees-of-freedom Air Bearing Spacecrafy Simulator ［D］.Harbin: Harbin Institute of Technology, 2010.(in Chinese)

[16] XU J, REN D, YANG Q J, et al.. The design of pneumatic cicuit for the 5-DOF air-bearing spacecraft simulator ［J］. Chinese Hydraulics & Pneumatics, 2009(9): 11-13.(in Chinese)

[17] LIU D, LIU Y H, CHEN SH J, et al.. Static Pressure Gas Lubrication ［M］. Harbin: Harbin Institute of Technology Press, 1990.(in Chinese)

[18] SONG G, BUCK N, AGRAWAL B, et al.. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper ［J］.Journal of Guidance Control & Dynamics, 1997, 22(3): 433-440.