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Volume 2 (2009)
Volume 1 (2008)
Author = M. Sayanjali
Number of Articles: 2
Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control
Volume 2, Issue 1 , April 2009, , Pages 43-50
Abstract
In this paper, equation of motion of three axis attitude dynamic of flexible spacecraft is derived using combination of finite element method and Euler equation. Flexible appendafes are modeled by beam elements. Goal of control is target attitude of spacecraft from initial state to desired attitude and ... Read MoreFlexible Spacecraft Attitude Control using Hybrid Control Scheme of Hâ and Sliding Mode Control
Volume 1, Issue 2 , December 2008, , Pages 51-56