Relative Orbit Geometry Through Classical Orbit Element Differences

By Hanspeter Schaub. 2004

187 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Astronomy and Astrophysics

View Paper: https://www.semanticscholar.org/paper/8e742823db17e1ae030e954e9eb4b19172c82e1b

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In Aerospace Engineering

1. Simone D'Amico
2. Joshua Sullivan

In Astronomy and Astrophysics

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): “The direct first-order mapping between nondimensional RTNframe relative position components and Keplerian orbital element differences (OEDs) was provided by Casotto [25] and Schaub [26] as δrRR f r f ≈ Δa a e 1 ecf sf η3 ΔM − 1 ecf cf η2 Δe δrRT f r f ≈ 1 ecf 2 η3 ΔM 2 ecf sf η2 Δe ciΔΩ Δω δrRN f r ”