Delta-V Earth-Gravity-Assist Trajectories with Hybrid Solar Electric–Photonic Propulsion
2021; American Institute of Aeronautics and Astronautics; Volume: 45; Issue: 1 Linguagem: Inglês
10.2514/1.g006136
ISSN1533-3884
Autores Tópico(s)Astro and Planetary Science
ResumoNo AccessEngineering NotesDelta-V Earth-Gravity-Assist Trajectories with Hybrid Solar Electric–Photonic PropulsionYuki Takao and Toshihiro ChujoYuki Takao https://orcid.org/0000-0003-1857-6449Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan and Toshihiro ChujoTokyo Institute of Technology, Tokyo 152-8550, JapanPublished Online:7 Oct 2021https://doi.org/10.2514/1.G006136SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Battin R. H., "The Determination of Round-Trip Planetary Reconnaissance Trajectories," Journal of the Aero/Space Sciences, Vol. 26, No. 9, 1959, pp. 545–567. https://doi.org/10.2514/8.8204 LinkGoogle Scholar[2] Casalino L., Colasurdo G. and Pastrone D., "Optimal Low-Thrust Escape Trajectories Using Gravity Assist," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 5, 1999, pp. 637–642. https://doi.org/10.2514/2.4451 LinkGoogle Scholar[3] Petropoulos A. E., Longuski J. M. and Bonfiglio E. P., "Trajectories to Jupiter via Gravity Assists from Venus, Earth, and Mars," Journal of Spacecraft and Rockets, Vol. 37, No. 6, 2000, pp. 776–783. https://doi.org/10.2514/2.3650 LinkGoogle Scholar[4] Wagner S. and Wie B., "Hybrid Algorithm for Multiple Gravity-Assist and Impulsive Delta-V Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 38, No. 11, 2015, pp. 2096–2107. https://doi.org/10.2514/1.G000874 LinkGoogle Scholar[5] Hollenbeck G. R., "New Flight Techniques for Outer Planet Missions," AIAA Conference on the Exploration of the Outer Planets, American Astronautical Society, AAS Paper 75-087, 1975. Google Scholar[6] Sweetser T. H., "Jacobi's Integral and ΔV-Earth-Gravity-Assist (ΔV-EGA) Trajectories," Advances in the Astronautical Sciences, Vol. 85, Aug. 1993, pp. 417–430. Google Scholar[7] Sims J. A., Longuski J. M. and Staugler A. J., "Leveraging for Interplanetary Missions: Multiple-Revolution Orbit Techniques," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3, 1997, pp. 409–415. https://doi.org/10.2514/2.4064 LinkGoogle Scholar[8] Casalino L., Colasurdo G. and Pastrone D., "Optimization of ΔV Earth-Gravity-Assist Trajectories," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 991–995. https://doi.org/10.2514/2.4336 LinkGoogle Scholar[9] Meissinger H., "Earth Swingby–A Novel Approach to Interplanetary Missions Using Electric Propulsion," AIAA 8th Electric Propulsion Conference, AIAA Paper 1970-1117, 1970. https://doi.org/10.2514/6.1970-1117 Google Scholar[10] Atkins K., Sauer C. and Flandro G., "Solar Electric Propulsion Combined with Earth Gravity Assist: A New Potential for Planetary Exploration," AIAA/AAS Astrodynamics Conference, AIAA Paper 1976-807, 1976. https://doi.org/10.2514/6.1976-807 Google Scholar[11] Kawaguchi J., "Solar Electric Propulsion Leverage: Electric Delta-VEGA (EDVEGA) Scheme and Its Application," 11th AAS/AIAA Space Flight Mechanics Meeting, American Astronautical Society, AAS Paper 01-213, 2001. Google Scholar[12] Kawaguchi J., "Performance Evaluation for the Electric Delta-V Earth Gravity Assist (EDVEGA) Scheme," AIAA/AAS Astrodynamics Specialist Conference and Exhibit, AIAA Paper 2002-4899, 2002. https://doi.org/10.2514/6.2002-4899 Google Scholar[13] Gong S. and Macdonald M., "Review on Solar Sail Technology," Astrodynamics, Vol. 3, No. 2, 2019, pp. 93–125. https://doi.org/10.1007/s42064-019-0038-x CrossrefGoogle Scholar[14] Heiligers J., Fernandez J. M., Stohlman O. R. and Wilkie W. K., "Trajectory Design for a Solar-Sail Mission to Asteroid 2016 HO 3," Astrodynamics, Vol. 3, No. 3, 2019, pp. 231–246. https://doi.org/10.1007/s42064-019-0061-1 CrossrefGoogle Scholar[15] Quarta A. A., Mengali G. and Bassetto M., "Optimal Solar Sail Transfers to Circular Earth-Synchronous Displaced Orbits," Astrodynamics, Vol. 4, No. 3, 2020, pp. 193–204. https://doi.org/10.1007/s42064-019-0057-x CrossrefGoogle Scholar[16] Kawaguchi J., Fujiwara A. and Uesugi T. K., "The Ion Engines Cruise Operation and the Earth Swingby of 'Hayabusa' (MUSES-C)," 55th International Astronautical Congress, International Astronautical Federation, Paper IAC 04-Q.5.02, 2004. https://doi.org/10.2514/6.IAC-04-Q.5.02 Google Scholar[17] Tsuda Y., Nakazawa S., Kushiki K., Yoshikawa M., Kuninaka H. and Watanabe S., "Flight Status of Robotic Asteroid Sample Return Mission Hayabusa2," Acta Astronautica, Vol. 127, Oct.–Nov. 2016, pp. 702–709. https://doi.org/10.1016/j.actaastro.2016.01.027 CrossrefGoogle Scholar[18] Tsuda Y., Mori O., Funase R., Sawada H., Yamamoto T., Saiki T., Endo T., Yonekura K., Hoshino H. and Kawaguchi J., "Achievement of IKAROS–Japanese Deep Space Solar Sail Demonstration Mission," Acta Astronautica, Vol. 82, No. 2, 2013, pp. 183–188. https://doi.org/10.1016/j.actaastro.2012.03.032 CrossrefGoogle Scholar[19] Vulpetti G., Johnson L. and Matloff G. L., "The NanoSAIL-D2 NASA Mission," Solar Sails, Springer, New York, 2015, pp. 173–178. Google Scholar[20] Mansell J., Spencer D. A., Plante B., Diaz A., Fernandez M., Bellardo J., Betts B. and Nye B., "Orbit and Attitude Performance of the LightSail 2 Solar Sail Spacecraft," AIAA Scitech 2020 Forum, AIAA Paper 2020-2177, 2020. https://doi.org/10.2514/6.2020-2177 Google Scholar[21] Baig S. and McInnes C. R., "Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion," Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, 2008, pp. 1644–1655. https://doi.org/10.2514/1.36125 LinkGoogle Scholar[22] Heiligers J., Ceriotti M., McInnes C. R. and Biggs J. D., "Displaced Geostationary Orbit Design Using Hybrid Sail Propulsion," Journal of Guidance, Control, and Dynamics, Vol. 34, No. 6, 2011, pp. 1852–1866. https://doi.org/10.2514/1.53807 LinkGoogle Scholar[23] Wilcox B. H., "Hybrids of Solar Sail, Solar Electric, and Solar Thermal Propulsion for Solar-System Exploration," 2012 IEEE Aerospace Conference, Institute of Electrical and Electronics Engineers, New York, 2012, pp. 1–8. https://doi.org/10.1109/AERO.2012.6187292 Google Scholar[24] Kawaguchi J., "A Solar Power Sail Mission for a Jovian Orbiter and Trojan Asteroid Flybys," 55th International Astronautical Congress, International Astronautical Federation, Paper IAC 04-Q.2.A.03, 2004. https://doi.org/10.2514/6.IAC-04-Q.2.A.03 Google Scholar[25] Ono G., Mimasu Y. and Kawaguchi J., "Delta-VEGA with a Spinning Solar Sail via Attitude and Spin Rate Control," 22nd Workshop on JAXA Astrodynamics and Flight Mechanics, Inst. of Space and Astronautical Science, Japan Aerospace Exploration Agency, Paper B-11, 2012. Google Scholar[26] McInnes C. R., Solar Sailing: Technology, Dynamics and Mission Applications, Springer Science & Business Media, New York, 2004, Chap. 2. Google Scholar[27] Takao Y., Mori O., Matsushita M. and Sugihara A. K., "Solar Electric Propulsion by a Solar Power Sail for Small Spacecraft Missions to the Outer Solar System," Acta Astronautica, Vol. 181, April 2021, pp. 362–376. https://doi.org/10.1016/j.actaastro.2021.01.020 CrossrefGoogle Scholar[28] Meng Y., Zhang H. and Gao Y., "Low-Thrust Minimum-Fuel Trajectory Optimization Using Multiple Shooting Augmented by Analytical Derivatives," Journal of Guidance, Control, and Dynamics, Vol. 42, No. 3, 2019, pp. 662–677. https://doi.org/10.2514/1.G003473 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 45, Number 1January 2022 CrossmarkInformationCopyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAsteroidsAstronomyCelestial Coordinate SystemCelestial MechanicsPlanetary Science and ExplorationPlanetsSolar PhysicsSpace AgenciesSpace MissionsSpace Science and Technology KeywordsEarthSolar Electric PropulsionGravity Assist TrajectoriesHybrid PropulsionPontryagin's Maximum PrincipleFuel ConsumptionDeep Space ManeuverSynchronous OrbitSpacecraft DesignOrbital PeriodAcknowledgmentThis work was supported by Grants-in-Aid for Scientific Research (20 J01938) from the Japan Society for the Promotion of Science.PDF Received19 April 2021Accepted28 August 2021Published online7 October 2021
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