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

By K. Yamanaka, F. Ankersen. 2002

640 citations recorded by the source corpus.

Subfields: Aerospace Engineering

View Paper: https://www.semanticscholar.org/paper/c5b8cf28607cf995540892ff9c236ca9ef05dd98

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In Aerospace Engineering

1. Simone D'Amico
2. Joshua Sullivan

Citations in the corpus

• Nonlinear Kalman Filtering for Improved Angles-Only Navigation Using Relative Orbital Elements (2017, methodology): “109) to compactly propagate the linearized solution developed by Yamanaka andAnkersen (YA) [28] for the relative position from a set of integration constants.”