Trajectory optimization using regularized variables.

DOI10.2514/3.5268zbMath0179.53502OpenAlexW1979338785MaRDI QIDQ5570698

B. D. Tapley, J. M. Lewallen, Victor Szebehely

Publication date: 1969

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2060/19690000667

Mathematics Subject Classification ID

Orbital mechanics (70M20) Collisions in celestial mechanics, regularization (70F16)

Related Items (4)

Optimal impulse space trajectories of a material point in the field of two bodies ⋮ A comparative study of Newtonian, Kustaanheimo/Stiefel, and Sperling/Burdet optimal trajectories ⋮ General time elements for the two body problem ⋮ Time elements in Keplerian orbital elements

This page was built for publication: Trajectory optimization using regularized variables.