Trajectory Optimization Using Nonsingular Orbital Elements and True Longitude

DOI10.2514/2.4147zbMath0888.70018OpenAlexW2018128618MaRDI QIDQ4364180

Jean Albert Kéchichian

Publication date: 13 November 1997

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

Full work available at URL: https://doi.org/10.2514/2.4147

zbMATH Keywords

adjoint equationsKepler's equationlow-thrust transferperturbation accelerationsrendezvous trajectoriesrotating polar frame

Mathematics Subject Classification ID

Differential games and control (49N70) Free motion of a rigid body (70E15) Orbital mechanics (70M20) Pursuit and evasion games (49N75)

Related Items (2)

Extended analytical formulae for the perturbed Keplerian motion under low-thrust acceleration and orbital perturbations ⋮ Optimization of low-thrust limited-power trajectories in a noncentral gravity field-transfers between orbits with small eccentricities

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