2008
DOI: 10.3103/s0025654408020027
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Evolution of the satellite fast rotation due to the gravitational torque in a dragging medium

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Cited by 17 publications
(8 citation statements)
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“…e moments of inertia I i , i � 1, 2, 3 are assumed as arbitrary constants that satisfy the above condition, and λ 3 is estimated by substituting (7) into the second equation from (4). is problem has wide applications in satellite motions which assumed moments of inertia according to the above relations [16][17][18]. A numerical example is given to show the stability conditions for a special case.…”
Section: Discussionmentioning
confidence: 99%
“…e moments of inertia I i , i � 1, 2, 3 are assumed as arbitrary constants that satisfy the above condition, and λ 3 is estimated by substituting (7) into the second equation from (4). is problem has wide applications in satellite motions which assumed moments of inertia according to the above relations [16][17][18]. A numerical example is given to show the stability conditions for a special case.…”
Section: Discussionmentioning
confidence: 99%
“…New analytical and simulation outcomes for CBFTs along the minor, middle, or major axes are presented. The rapid rotational motions of unbalanced asymmetric satellites around their center of mass under the influence of both gravitational and drag torques are examined in 4 . It is concluded that the satellites’ kinetic energy and angular momentum decrease, in which they are identified in the presence of Quasi stationary motion phases.…”
Section: Introductionmentioning
confidence: 99%
“…In the last few decades, many researchers have focused their work on studying the RB's motion when the applied external torques have various types. [1][2][3][4][5][6][7][8][9][10] The main factor of this progress is due to its broad range of uses in diverse fields, including satellites, spacecraft, and the like. An investigation of an asymmetrical satellite's motion under the action of pressure forces and resistive moments is presented in Ref.…”
Section: Introductionmentioning
confidence: 99%
“…More contributions to this problem are discussed in Ref. 4 when the satellite is subjected to both drag and gravitational force. The authors considered that the drag torque is linearly related to the satellite’s angular velocity.…”
Section: Introductionmentioning
confidence: 99%