On bounded satellite motion under constant radial propulsive acceleration
From MaRDI portal
Publication:1955072
DOI10.1155/2012/680394zbMath1264.70043OpenAlexW2022847476WikidataQ58911573 ScholiaQ58911573MaRDI QIDQ1955072
Publication date: 11 June 2013
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2012/680394
Completely integrable systems and methods of integration for problems in Hamiltonian and Lagrangian mechanics (70H06) Celestial mechanics (70F15) Orbital mechanics (70M20)
Related Items (3)
DROMO formulation for planar motions: solution to the Tsien problem ⋮ Fourier series approximations to \(J_2\)-bounded equatorial orbits ⋮ Multiple scales asymptotic solution for the constant radial thrust problem
Cites Work
- Unnamed Item
- Analytical results for solar sail optimal missions with modulated radial thrust
- Families of canonical transformations by Hamilton-Jacobi-Poincaré equation. Application to rotational and orbital motion
- Some generalized Penrose patterns from projections ofn-dimensional lattices
- The elimination of the parallax in satellite theory
This page was built for publication: On bounded satellite motion under constant radial propulsive acceleration
