A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary
From MaRDI portal
Publication:1637799
DOI10.1007/s10569-017-9806-4zbMath1390.70059OpenAlexW2791911678MaRDI QIDQ1637799
Ashley D. Biria, Ryan P. Russell
Publication date: 11 June 2018
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-017-9806-4
Related Items (2)
A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary ⋮ The Lagrange coefficients of Vinti theory
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Satellite relative motion using differential equinoctial elements
- Canonical modelling of relative spacecraft motion via epicyclic orbital elements
- Second-order state transition for relative motion near perturbed, elliptic orbits
- Integrable systems in celestial mechanics.
- A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary
- Integrable approximation of \(J_2\)-perturbed relative orbits
- Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations
- Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
- An analytic solution for theJ 2 perturbed equatorial orbit
- Note on Cid's radial intermediary and the method of averaging
- State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
- The extended phase space formulation of the Vinti problem
- Polynomial Roots from Companion Matrix Eigenvalues
- Theory of an accurate intermediary orbit for satellite astronomy
- Intermediary equatorial orbits of an artificial satellite
- Invariant properties of the spheroidal potential of an oblate planet
- Inclusion of the third zonal harmonic in an accurate reference orbit of an artificial satellite
- Improvement of mean orbital elements for Vinti's spheroidal satellite theory.
- Zonal harmonic perturbations of an accurate reference orbit of an artificial satellite
- \(J_2\) invariant relative orbits for spacecraft formations
This page was built for publication: A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary
