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مقاله‌ی دسترسی آزاد

Rapid Low-Thrust Trajectory Optimization in Deep Space Based on Convex Programming

['Christian Hofmann', 'Francesco Topputo', '']

چکیده

No AccessEngineering NotesRapid Low-Thrust Trajectory Optimization in Deep Space Based on Convex ProgrammingChristian Hofmann and Francesco TopputoChristian HofmannPolytechnic University of Milan, 20156 Italy*Ph.D. Candidate, Department Aerospace Science Technology, Via La Masa 34; .Search for more papers by this author Topputo https://orcid.org/0000-0002-5369-6887Polytechnic Italy†Associate Professor, . Senior Member AIAA.Search authorPublished Online:30 Apr 2021https://doi.org/10.2514/1.G005839SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Pontani M. Conway B. A., “Particle Swarm Applied Trajectories,” Journal Guidance, Control, Dynamics, Vol. 33, No. 5, 2010, pp. 1429–1441. https://doi.org/10.2514/1.48475 LinkGoogle Scholar[2] Zhang C., F., Bernelli-Zazzera F. Zhao Y. 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All rights reserved. requests copying permission reprint should be submitted CCC at www.copyright.com; employ eISSN 1533-3884 initiate your request. See also Rights Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAlgorithms Data StructuresArtificial IntelligenceComputational Fluid DynamicsComputing, Information, CommunicationData ScienceEvolutionary AlgorithmFluid DynamicsMachine LearningNumerical AnalysisOptimization AlgorithmPseudospectral KeywordsThrustTrajectory OptimizationEarthNumerical OptimizationPseudospectral MethodsNonlinear DynamicsSmall SatellitesSparse OptimizerNumerical SimulationAsteroidsPDF Received4 2020Accepted22 February 2021Published online30 April

اسناد مشابه

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