An intelligent control concept for formation flying satellites

DOI10.1002/rnc.678zbMath1098.70542OpenAlexW2080592166MaRDI QIDQ4532962

Sesha Sai Vaddi, Srinivas R. Vadali, Kyle T. Alfriend

Publication date: 2002

Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/rnc.678

zbMATH Keywords

initial conditionsformation flyingreference trajectorydisturbance accommodation

Mathematics Subject Classification ID

Automated systems (robots, etc.) in control theory (93C85) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (9)

Cluster flight control for fractionated spacecraft on an elliptic orbit ⋮ Second-order state transition for relative motion near perturbed, elliptic orbits ⋮ Symmetry properties of optimal relative orbit trajectories ⋮ Analytical solutions of the relative orbital motion in unperturbed and in J ₂ - perturbed elliptic orbits ⋮ Nonlinear analytic solution for perturbed relative motion using differential equinoctial elements ⋮ Minimum control for spacecraft formations in a J2 perturbed environment ⋮ Application of Hamiltonian structure-preserving control to formation flying on a \(J_2\)-perturbed mean circular orbit ⋮ Finite‐Time Optimal Formation Control for Second‐Order Multiagent Systems ⋮ Finite-time optimal formation control of multi-agent systems on the Lie group SE(3)

Cites Work

• Long-Term Formation Keeping of Satellite Constellation Using Linear-Quadratic Controller

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