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Close approach of a cloud of particles around an oblate planet

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Abstract

The goal of the present paper is to study close approaches of a cloud of particles with an oblate planet, which means that there is a \(J_{2}\) term in the gravitational potential of the planet. This cloud of particles is assumed to be created during the passage of a spacecraft by the periapsis of its orbit, by an explosion or any other disruptive event. The system is formed by two large bodies (Sun and planet), assumed to be in circular orbits around the center of mass of the system, and the cloud of particles. The particles that belong to the cloud make a close approach to the flat planet and then they are dispersed by the gravitational force of the planet. The motion is governed by the equations of motion given by the planar restricted circular three-body problem plus the effects of the oblateness of the planet. Jupiter is used for numerical simulations. The results show the differences between the behavior of the cloud after the passage, considering or not the effects of the oblateness of the planet. The results show that the oblateness of the planet is equivalent to an increase in the mass of the planet.

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References

  • Broucke RA (1988) The celestial mechanics of gravity assist. AIAA paper 88-4220. In: AIAA/AAS astrodynamics conference, Minneapolis, MN, 15–17 Aug

  • Brouwer D, Clemence G (1961) Methods of celestial mechanics. Academic Press, Massachusetts

    MATH  Google Scholar 

  • Byrnes DV, D’Amario LA (1982) A combined Halley flyby Galileo mission. AIAA paper, 82-1462

  • Carvell R (1986) Ulysses—the Sun from above and below. Space 1:18

    Google Scholar 

  • Casalino L, Colasurdo G, Pastrone D (1999) Optimal low-thrust escape trajectories using gravity assist. J Guidance Control Dyn 22(5):637–642

    Article  Google Scholar 

  • D’Amario LA, Byrnes DV (1983) Interplanetary trajectory design for the Galileo mission. In: AIAA, aerospace sciences meeting, vol 1

  • D’Amario LA, Sackett LL, Stanford RH, Byrnes DV (1979) Optimization of multiple flyby trajectories. In: American Institute of Aeronautics and Astronautics conference, vol 1

  • D’Amario LA, Byrnes DV, Stanford RH (1981) A new method for optimizing multiple-flyby trajectories. J Guidance Control Dyn 4(5):591–596

    Article  Google Scholar 

  • D’Amario LA, Byrnes DV, Stanford RH (1982) Interplanetary trajectory optimization with application to Galileo. J Guidance Control Dyn 5(5):465–471

    Article  Google Scholar 

  • Farquhar RW, Dunham DW (1981) A new trajectory concept for exploring the Earth’s geomagnetic tail. J Guidance Control Dyn 4(2):192–196

    Article  Google Scholar 

  • Gomes VM, Prado AFBA (2008) Swing-by maneuvers for a cloud of particles with planets of the solar system. WSEAS Trans Appl Theor Mech 3(11):869–878

    Google Scholar 

  • Gomes VM, Prado AFBA (2010) A study of the impact of the initial energy in a close approach of a cloud of particles. WSEAS Trans Math 9(10):811–820

    Google Scholar 

  • Gomes VM, Prado AFBDA, Golebiewska J (2013) Dynamics of space particles and spacecrafts passing by the atmosphere of the Earth. Sci World J 2013:1–6

  • Heaton AF, Strange NJ, Longuski JM, Bonfiglio EP (2002) Automated design of the Europa Orbiter tour. J Spacecr Rockets 39(1):17–22

    Article  Google Scholar 

  • Hollister WM, Prussing JE (1966) Optimum transfer to Mars via Venus (transfer paths to Mars via Venus compared with direct flight, discussing direct free fall transfer, flyby and free fall transfer). Astronaut Acta 12:169–179

    Google Scholar 

  • Kohlhase CE, Penzo PA (1977) Voyager mission description. Space Sci Rrev 21(2):77–101

    Google Scholar 

  • Lanoix E (1996) Tether sling shot assists—a novel approach to travelling in the solar system. In: CASI conference on astronautics—towards the next century in space, 9th, Ottawa, Canada, pp 62–71

  • Lanoix ELM, Misra AK (2000) Near-earth asteroid missions using tether sling shot assist. J Spacecr Rockets 37(4):475–480

    Article  Google Scholar 

  • Longman RW, Schneider AM (1970) Use of Jupiter’s moons for gravity assist. J Spacecr Rockets 7(5):570–576

    Article  Google Scholar 

  • Longuski JM, Williams SN (1991) The last grand tour opportunity to Pluto. J Astronaut Sci 39:359–365

    Google Scholar 

  • Marsh SM, Howell KC (1988) Double lunar swingby trajectory design. AIAA paper, 88-4289

  • McConaghy TT, Debban TJ, Petropoulos AE, Longuski JM (2003) Design and optimization of low-thrust trajectories with gravity assists. J Spacecr Rockets 40(3):380–387

    Article  Google Scholar 

  • Penzo PA, Mayer HL (1986) Tethers and asteroids for artificial gravity assist in the solar system. J Spacecr Rockets 23(1):79–82

    Article  Google Scholar 

  • Prado AFBA, Broucke R (1995a) Classification of swing-by trajectories using the Moon. Appl Mech Rev 48(11S):S138–S142

    Article  Google Scholar 

  • Prado AFBA, Broucke R (1995b) Effects of atmospheric drag in swing-by trajectory. Acta Astronaut 36(6):285–290

    Article  Google Scholar 

  • Puig-Suari J, Longuski JM, Tragesser SG (1995) A tether sling for lunar and interplanetary exploration. Acta Astronaut 35:671–680

    Article  MATH  Google Scholar 

  • Sanchez DM, Yokoyama T, Brasil PIDO, Cordeiro RR (2009) Some initial conditions for disposed satellites of the systems GPS and Galileo constellations. Math Probl Eng 2009:510759. doi:10.1155/2009/510759

  • Strange NJ, Longuski JM (2002) Graphical method for gravity-assist trajectory design. J Spacecr Rockets 39(1):9–16

    Article  Google Scholar 

  • Striepe SA, Braun RD (1991) Effects of a Venus swingby periapsis burn during an Earth-Mars trajectory. J Astronaut Sci 39(3):299–312

  • Sukhanov AA (1999) Close approach to Sun using gravity assists of the inner planets. Acta Astronaut 45(4):177–185

    Article  MathSciNet  Google Scholar 

  • Swenson BL (1992) Neptune atmospheric probe mission. AIAA paper (92-4371)

  • Szebehely VG (1967) Theory of orbits. Academic Press, New York

    Google Scholar 

  • Thompson WB, Stern MO, Dubin DHE (1998) A skyhook from Phobos to Mars. J Br Interplanet Soc 51(3):99–115

    Google Scholar 

Download references

Acknowledgments

The authors wish to express their appreciation for the support provided by Grants # 473387/2012-3, 304700/2009-6 and 473164/2013-2 from the National Council for Scientific and Technological Development (CNPq); Grants # 2011/08171-3, 2011/13101-4, 2014/06688-7, 2012/21023-6 and 2014/22295-5 from São Paulo Research Foundation (FAPESP) and the financial support from the National Council for the Improvement of Higher Education (CAPES).

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Correspondence to Diogo M. Sanchez.

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Communicated by Elbert E. N. Macau, Antônio Fernando Bertachini de Almeida Prado and Cristiano Fiorilo de Melo.

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Gomes, V.M., Oliveira, G.M.C., Prado, A.F.B.A. et al. Close approach of a cloud of particles around an oblate planet. Comp. Appl. Math. 35, 663–673 (2016). https://doi.org/10.1007/s40314-015-0264-x

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  • DOI: https://doi.org/10.1007/s40314-015-0264-x

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