Low-Thrust Minimum-Fuel Optimization in the Circular Restricted Three-Body Problem
2015; American Institute of Aeronautics and Astronautics; Volume: 38; Issue: 8 Linguagem: Inglês
10.2514/1.g001080
ISSN1533-3884
AutoresChen Zhang, Francesco Topputo, F. Bernelli Zazzera, Yushan Zhao,
Tópico(s)Astro and Planetary Science
ResumoNo AccessEngineering NoteLow-Thrust Minimum-Fuel Optimization in the Circular Restricted Three-Body ProblemChen Zhang, Francesco Topputo, Franco Bernelli-Zazzera and Yu-Shan ZhaoChen ZhangSchool of Astronautics, Beihang University, 100191 Beijing, People’s Republic of China*Ph.D. Candidate, School of Astronautics; .Search for more papers by this author, Francesco TopputoDepartment of Aerospace Science and Technolgy, Politecnico di Milano, 20156 Milan, Italy†Assistant Professor, Department of Aerospace Science and Technolgy; .Search for more papers by this author, Franco Bernelli-ZazzeraDepartment of Aerospace Science and Technolgy, Politecnico di Milano, 20156 Milan, Italy‡Professor, Department of Aerospace Science and Technology; .Search for more papers by this author and Yu-Shan ZhaoSchool of Astronautics, Beihang University, 100191 Beijing, People’s Republic of China§Professor, School of Astronautics; .Search for more papers by this authorPublished Online:12 Mar 2015https://doi.org/10.2514/1.G001080SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Mingotti G., Topputo F. and Bernelli-Zazzera F., “Optimal Low-Thrust Invariant Manifold Trajectories via Attainable Sets,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 6, 2011, pp. 1644–1656. doi:https://doi.org/10.2514/1.52493 JGCDDT 0162-3192 LinkGoogle Scholar[2] Mingotti G. and Gurfil P., “Mixed Low-Thrust Invariant-Manifold Transfers to Distant Prograde Orbits Around Mars,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 6, 2010, pp. 1753–1764. doi:https://doi.org/10.2514/1.49810 JGCDDT 0162-3192 LinkGoogle Scholar[3] Anderson R. and Lo M., “Role of Invariant Manifolds in Low-Thrust Trajectory Design,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 6, 2009, pp. 1921–1930. doi:https://doi.org/10.2514/1.37516 JGCDDT 0162-3192 LinkGoogle Scholar[4] Mingotti G., Topputo F. and Bernelli-Zazzera F., “Low-Energy, Low-Thrust Transfers to the Moon,” Celestial Mechanics and Dynamical Astronomy, Vol. 105, Nos. 1–3, 2009, pp. 61–74. doi:https://doi.org/10.1007/s10569-009-9220-7 CrossrefGoogle Scholar[5] Mingotti G., Topputo F. and Bernelli-Zazzera F., “Efficient Invariant-Manifold, Low-Thrust Planar Trajectories to the Moon,” Communications in Nonlinear Science and Numerical Simulation, Vol. 17, No. 2, 2012, pp. 817–831. doi:https://doi.org/10.1016/j.cnsns.2011.06.033 CrossrefGoogle Scholar[6] Pierson B. and Kluever C., “Three-Stage Approach to Optimal Low-Thrust Earth–Moon Trajectories,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, 1994, pp. 1275–1282. doi:https://doi.org/10.2514/3.21344 JGCDDT 0162-3192 LinkGoogle Scholar[7] Kluever C. and Pierson B., “Optimal Low-Thrust Three-Dimensional Earth–Moon Trajectories,” Journal of Guidance, Control, and Dynamics, Vol. 18, No. 4, 1995, pp. 830–837. doi:https://doi.org/10.2514/3.21466 JGCDDT 0162-3192 LinkGoogle Scholar[8] Herman A. and Conway B., “Optimal, Low-Thrust, Earth–Moon Orbit Transfer,” Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, 1998, pp. 141–147. doi:https://doi.org/10.2514/2.4210 JGCDDT 0162-3192 LinkGoogle Scholar[9] Russell R., “Primer Vector Theory Applied to Global Low-Thrust Trade Studies,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 2, 2007, pp. 460–472. doi:https://doi.org/10.2514/1.22984 JGCDDT 0162-3192 LinkGoogle Scholar[10] Caillau J., Daoud B. and Gergaud J., “Minimum Fuel Control of the Planar Circular Restricted Three-Body Problem,” Celestial Mechanics and Dynamical Astronomy, Vol. 114, Nos. 1–2, 2012, pp. 137–150. doi:https://doi.org/10.1007/s10569-012-9443-x CrossrefGoogle Scholar[11] Schoenmaekers J., Horas D. and Pulido J., “SMART-1: With Solar Electric Propulsion to the Moon,” Proceeding of the 16th International Symposium on Space Flight Dynamics, NASA Jet Propulsion Lab., Pasadena, CA, 2001, pp. 1–14. 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