Indirect Optimization of Power-Limited Asteroid Rendezvous Trajectories

No AccessEngineering NotesIndirect Optimization of Power-Limited Asteroid Rendezvous TrajectoriesYang Wang and Francesco TopputoYang WangPolytechnic University Milan, 20156 Italy*Ph.D. Candidate, Department Aerospace Science Technology, Via La Masa 34; (Corresponding Author).Search for more papers by this author Topputo https://orcid.org/0000-0002-5369-6887Polytechnic Italy†Full Professor, . Senior Member AIAA.Search authorPublished Online:14 Feb 2022https://doi.org/10.2514/1.G006179SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Quadrelli M., Wood L., Riedel J., McHenry Aung Cangahuala Volpe R., Beauchamp P. 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TopicsAsteroidsBoundary Element MethodComputational Fluid DynamicsFluid Flow PropertiesNumerical AnalysisPlanetary ExplorationPlanetsRunge-Kutta MethodsSpace MissionsSpace TechnologyTerminal Velocity KeywordsAsteroidsTransversality ConditionEarthSolar PropulsionLagrange PointsPropellantHamiltonian FunctionsRunge Kutta IntegrationBoundary Value ProblemsNonlinear ProgrammingAcknowledgmentPart work has been funded ESA through contract 4000127373/19/NL/AF (M-ARGO mission Phase study).PDF Received4 May 2021Accepted11 January 2022Published online14 February