[1]
P. Kumar, and; S. Pellegrino, Deployment and retraction of a cable-driven solar array: testing and simulation, NTRS report.
Google Scholar
[2]
J. M. A. Scherpen , B. Van Der Kerk , J. B. Klaassens , M. Lazeroms , and S. Y. Kan, Nonlinear Control for Magnetic Bearings in Deployment Test Rigs: Simulation and Experimental Results, presented at the 37th IEEE Conf. on decision and control, Tampa, FL, USA, December 6-18, (1998).
DOI: 10.1109/cdc.1998.757846
Google Scholar
[3]
A. Fischer, and S. Pellegrino, Interaction Between Gravity Compensation Suspension System and Deployable Structure, Journal of spacecrafts and rockets, 37(1), pp, 93-99.
DOI: 10.2514/2.3531
Google Scholar
[4]
H.B. Brown, Jr. and J.M. Dolan, A novel gravity compensation system for space robots, ASCE Specialty Conf. on Robotics for Challenging Environments, Albuquerque, NM, USA, pp.250-258, (1994).
Google Scholar
[5]
A. Kemurdjian, Development of simulation means for a gravity forces, presented at the American Society of Civil Engineers, Albuquerque, New Mexico, Feb 27-Mar 2, 2000, Robotics2000, pp.220-225.
Google Scholar
[6]
G. C. White, Y. S. Xu, An active vertical-direction gravity compensation system, IEEE Transactions on instrumentation and measurement, vol. 43, issue 6, Decenber 1994, pp.786-792, (1994).
DOI: 10.1109/19.368066
Google Scholar
[7]
Sato, Yuichi, Ejiri, Arata, and Iida etc., Micro-G Emulation System Using Constant-Tension Suspension for a Space Manipulator, presented at IEEE International Conference on Robotics and Automation, CA, USA, April 9-11, 1991, volume 3, p.1893-(1900).
DOI: 10.1109/robot.1991.131902
Google Scholar
[8]
Lockheed Missile & Space Company, Condensed Summary Report: Preliminary Design Study of A Lunar Gravity Simulator, NTRS report, (1967).
Google Scholar