Closed form parametric solutions of nonlinear Abel-type and Riccati-type spacecraft relative motion
Author:
Funder
Aerospace Engineering Department of Auburn University
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. Terminal guidance for satellite rendezvous;Clohessy;J. Aerosp. Sci.,1960
2. Analytical Mechanics of Space Systems;Schaub,2014
3. Comprehensive survey and assessment of spacecraft relative motion dynamics models;Sullivan;J. Guid. Control Dyn.,2017
4. Second approximation to the solution of the rendezvous equations;London;AIAA J.,1963
5. Rendezvous problem for nearly circular orbits;Anthony;AIAA J.,1965
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