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Simo, Jules; McInnes, Colin R.
Languages: English
Types: Other

Classified by OpenAIRE into

arxiv: Physics::Space Physics, Astrophysics::Earth and Planetary Astrophysics, Quantitative Biology::Other, Physics::Popular Physics
Solar sail technology offers new capabilities for space missions due to the opportunities\ud for non-Keplerian orbits. In this paper, novel families of highly non-Keplerian orbits\ud for spacecraft utilising solar sail at linear order are investigated in the Earth-Moon\ud circular restricted three-body problem. Firstly, it is assumed implicitly that the solar\ud sail is a perfect reflector. Based upon the first-order approximation, an analytical formulation\ud of the periodic orbits at linear order is presented. The approximate analytical\ud solutions offer useful insights into the nature of the motion in the vicinity of the libration\ud points, and are used to give periodic solutions numerically in the full nonlinear\ud system. These orbits were accomplished by using an optimal choice of the sail pitch\ud angle, which maximize the out-of-plane distance. Thereafter, the resulting effects of\ud the non-ideal flat sail model have been computed and compared with an ideal solar\ud sail. A square sail configuration, which is likely to be chosen for various near-term sail\ud missions is used to illustrate the concept. The main effect of the non-perfect sail is to\ud reduce the out-of-plane displacement distance which may be achieved for a given\ud characteristic acceleration. It is also observed that there is a significant deviation in\ud force magnitude between the realistic solar sail and the ideal solar sail model.
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    • [1] J. Simo and C. R. McInnes, “Solar sail trajectories at the Earth-Moon Lagrange points,” In 59th International Astronautical Congress, Glasgow, Scotland, 29 Sep - 03 Oct 2008. Paper IAC-08.C1.3.13.
    • [2] J. Simo and C. R. McInnes, “Solar Sail Orbits at the Earth-Moon Libration points,” Communications in Nonlinear Science and Numerical Simulation, Vol. 14, No. 12, December 2009, pp. 4191-4196.
    • [3] J. Simo and C. R. McInnes, “Designing Displaced Lunar Orbits Using Low-Thrust Propulsion,” Journal of Guidance, Control and Dynamics, Vol. 33, No. 1, January-February 2010.
    • [4] J. Simo and C. R. McInnes, “Displaced solar sail orbits: Dynamics and applications,” In 20th AAS/AIAA Space Flight Mechanics Meeting, San Diego, California, February 14-17, 2010. AAS 10-222.
    • [5] J. Simo and C. R. McInnes, “Tracking Unstable Periodic Orbits in the Circular Restricted Three-Body Problem,” Workshop on Applications on Control theory to Astrodynamics problems, Surrey, England, April 26-27, 2010.
    • [6] J. Simo and C. R. McInnes, “Feedback Stabilization of Displaced Periodic Orbits: Application to Binary Asteroids,” Acta Astronautica, Vol. 96, March-April 2014, pp. 106-115.
    • [7] C. R. McInnes, Solar sailing: technology, dynamics and mission applications. London: Springer Praxis, 1999.
    • [8] M. Leipold and M. Go¨tz, “Hybrid Photonic/Electric Propulsion,” Kayser-Threde, TR SOL4- TR-KTH0001, Munich, Jan. 2002, ESA Contract No. 15334/01/NL/PA.
    • [9] G. Mengali and A. A. Quarta, “Trajectory Design with Hybrid Low-Thrust Propulsion system,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 2, March-April 2007, pp. 419-426.
    • [10] B. Wie, “Thrust Vector Control Analysis and Design for Solar-Sail Spacecraft,” Journal of Spacecraft and Rockets, Vol. 44, No. 3, May-June 2007, pp. 545-557.
    • [11] V. L. Coverstone and J. E. Prussing, “Technique for Escape from Geosynchronous Transfer Orbit Using a Solar Sail,” Journal of Guidance, Control and Dynamics, Vol. 26, No. 4, July-August 2003, pp. 628- 634.
    • [12] T. Cichan and R. G. Melton, “Optimal Trajectories for Non-Ideal Solar Sails,” Advances in the Astronautical Sciences, Vol. 109, No. 3, 2001, pp. 2381-2391.
    • [13] B. Dachwald, W. Seboldt, and B. Ha¨usler, “Performance Requirements for Near-Term Interplanetary Solar Sailcraft Missions,” 6th International Symposium on Propulsion for Space Transportation of the XXIst Century, Versailles, France, May 2002.
    • [14] H. Baoyin and C. McInnes, “Solar sail halo orbits at the Sun-Earth artificial L1 point,” Celestial Mechanics and Dynamical Astronomy, Vol. 94, No. 2, 2006, pp. 155-171.
    • [15] J. Simo and C. R. McInnes, “Stabilization of Displaced Periodic Orbits in the Solar Sail Restricted Three-Body Problem,” presented at the SIAM Conference on Applications of Dynamical Systems (DS09), Snowbird, Utah, May 17 - 21, 2009.
    • [16] J. Simo and C. R. McInnes, “Asymptotic Analysis of Displaced Lunar Orbits,” Journal of Guidance, Control and Dynamics, Vol. 32, No. 5, September-October 2009, pp. 1666-1671.
    • [17] J. Simo and C. R. McInnes, “Analysis and Control of Displaced Periodic Orbits in the Earth-Moon System,” In 60th International Astronautical Congress, Daejeon, Republic of Korea, 12 - 16 October 2009. IAC-09.C1.2.4.
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