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Optimal Control of a Circular Satellite Formation Subject to Gravitational Perturbations60,99 €![An Analytical Study of T-38 Drag Reduction in Tight Formation Flight]( "An Analytical Study of T-38 Drag Reduction in Tight Formation Flight")
An Analytical Study of T-38 Drag Reduction in Tight Formation Flight60,99 €![Estimation of Relative Satellite Formation Element Positions in Near Circular Orbits]( "Estimation of Relative Satellite Formation Element Positions in Near Circular Orbits")
Estimation of Relative Satellite Formation Element Positions in Near Circular Orbits60,99 €![Estimation of Relative Satellite Formation Element Positions in Near Circular Orbits]( "Estimation of Relative Satellite Formation Element Positions in Near Circular Orbits")
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Performance Analysis of Protocol Independent Multicasting-Dense Mode in Low Earth Orbit Satellite Networks60,99 €![Comparative Analysis of Mobility Management Schemes in a Low Earth Orbit Satellite Network]( "Comparative Analysis of Mobility Management Schemes in a Low Earth Orbit Satellite Network")
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Satellite formations or distributed satellite systems provide advantages not feasible with single satellites. Efficient operation of this platform requires the use of optimal control of the entire satellite formation. While the optimal control theory is well established, only a very simple dynamical system affords an analytical solution. Any practical optimal control problem solve the resulting two-point boundary value (TPBV) problem numerically. In this research, the optimization of satellite formation control is solved analytically. The relative satellite dynamics using Hill's coordinate system and approximations made by Clohessy and Wiltshire, combined with body-fixed thruster control, result in a linearized dynamic system.