New approach to halo orbit determination and control

DOI10.2514/3.21614zbMath0851.70010OpenAlexW2001484590MaRDI QIDQ4884797

David Cielaszyk, Bong Wie

Publication date: 28 November 1996

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.21614

zbMATH Keywords

circular restricted three-body problemlibration pointiterative numerical methodfuel-efficient nominal pathlinear state-feedback controllerLissajous trajectory

Mathematics Subject Classification ID

Three-body problems (70F07) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (6)

Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems ⋮ A new control law based on characteristic exponent assignment for libration point orbit maintenance ⋮ Robust control of the Hill's problem with drag ⋮ Modified Chebyshev-Picard iteration methods for station-keeping of translunar halo orbits ⋮ Stabilization of Lagrange points in circular restricted three-body problem: a port-Hamiltonian approach ⋮ Floquet-based design and control approach to spacecraft formation flying in libration point orbits

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