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New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit Koji Yamanaka and Finn Ankersen

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A new state transition matrix is described for the nonlinear problem of relative motion on an arbitrary elliptical orbit A linearization is

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ADS New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit Yamanaka Koji Ankersen Finn Publication

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New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit Koji Yamanaka

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New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit Journal of Guidance Control and Dynamics 25 1

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New and simpler solution to those equations is represented in a convenient state transition matrix form This new state transition

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What s more we tried our new state transition matrix and found that the time delay exists in the new solution which is shown in

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This paper presents new state transition matrices that model the relative motion of two spacecraft in arbitrarily eccentric orbits

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Therefore a new state transition matrix STM of relative motion for elliptic reference orbits with J2 perturbation is considered in this