A procedure for the solution of Lambert's orbital boundary-value problem
From MaRDI portal
Publication:917339
zbMath0704.70004MaRDI QIDQ917339
Publication date: 1990
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Halley's cubic iterationkinematic geometrythree Fortran-77 subroutinesuniversal solution for Lambert's problem
Experimental work for problems pertaining to mechanics of particles and systems (70-05) Kinematics of a particle (70B05)
Related Items (12)
A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight ⋮ A projective approach to orbit determination from three sight-lines ⋮ Solution algorithm of a quasi-Lambert's problem with fixed flight-direction angle constraint ⋮ Orbital maneuver optimization using time-explicit power series ⋮ On the Lambert problem with drag ⋮ How many Keplerian arcs are there between two points of spacetime? ⋮ Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory ⋮ A closed-form solution to the minimum \(\Delta V_{\text{tot}}^{2}\) Lambert's problem ⋮ On universal elements, and conversion procedures to and from position and velocity ⋮ On the solution to every Lambert problem ⋮ Unconstrained direct optimization of spacecraft trajectories using many embedded Lambert problems ⋮ Revisiting Lambert's problem
This page was built for publication: A procedure for the solution of Lambert's orbital boundary-value problem