Cluster flight control for fractionated spacecraft on an elliptic orbit
From MaRDI portal
Publication:315247
DOI10.1007/S10569-016-9685-0zbMath1345.70047OpenAlexW2341236626MaRDI QIDQ315247
Yuying Liang, Tian Tan, Ming Xu, Li-Xin Wei
Publication date: 19 September 2016
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-016-9685-0
bounded and quasi-periodic relative trajectoriescluster flightelliptic orbitFloquet stabilityHamiltonian structure-preserving control
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Threshold result for semilinear parabolic equations with indefinite non-homogeneous term
- Nonlinear dynamical analysis for displaced orbits above a planet
- Analytical solution for power-limited optimal rendezvous near an elliptic orbit
- Introduction to Hamiltonian dynamical systems and the \(N\)-body problem.
- Application of Hamiltonian structure-preserving control to formation flying on a \(J_2\)-perturbed mean circular orbit
- Displaced orbits generated by solar sails for the hyperbolic and degenerated cases
- KAM stability and celestial mechanics
- State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
- An intelligent control concept for formation flying satellites
This page was built for publication: Cluster flight control for fractionated spacecraft on an elliptic orbit