Kumar, K and Pradeep, S (1998) Strategies for three dimensional deployment of tethered satellites. In: Mechanics Research Communications, 25 (5). pp. 543-550.
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Tethered satellites deployed from the Space Shuttle have been proposed for diverse applications. A funda- mental issue in the utilization of tethers is quick deployment and retrieval of the attached payload. Inordinate librations of the tether during deployment and retrieval is undesirable. The structural damping present in the system is too low to contain the librations. Rupp  proposed to control the tether reel located in the parent spacecraft to alter the tension in the tether, which in turn changes the stiffness and the damping of the system. Baker applied the tension control law to a model which included out of plane motion. Modi et al. proposed a control law that included nonlinear feedback of the out-of plane tether angular rate. More recently, nonlinear feedback control laws based on Liapunov functions have been proposed. Two control laws are derived in . The first is based on partial decomposition of the equations of motion and utilization of a two dimensional control law developed in . The other is based on a Liapunov function that takes into consideration out-of-plane motion. It is shown that the control laws are effective when used in conjunction with out-of-plane thrusting. Fujii et al., used the mission function control approach to study the control law including aerodynamic drag effect explicitly into the control algorithm.
|Item Type:||Journal Article|
|Additional Information:||Copyright of this article belongs to Elsevier Science.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||17 Dec 2009 12:19|
|Last Modified:||19 Sep 2010 05:27|
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