Simo, J. and McInnes, C.R. (2010) Displaced solar sail orbits: dynamics and applications. In: 20th AAS/AIAA Space Flight Mechanics Meeting, 2010-02-14 - 2010-02-17, San Diego, California.
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We consider displaced periodic orbits at linear order in the circular restricted Earth-Moon system, where the third massless body is a solar sail. These highly non-Keplerian orbits are achieved using an extremely small sail acceleration. Prior results have been developed by using an optimal choice of the sail pitch angle, which maximises the out-of-plane displacement. In this paper we will use solar sail propulsion to provide station-keeping at periodic orbits around the libration points using small variations in the sail's orientation. By introducing a first-order approximation, periodic orbits are derived analytically at linear order. These approximate analytical solutions are utilized in a numerical search to determine displaced periodic orbits in the full nonlinear model. Applications include continuous line-of-sight communications with the lunar poles.
|Item type:||Conference or Workshop Item (Paper)|
|Keywords:||solar sail orbits, out-of-plane displacement, libration points, first-order approximation, nonlinear model, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering, Control and Systems Engineering, Computational Mechanics|
|Subjects:||Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. Astronautics
|Department:||Faculty of Engineering > Mechanical and Aerospace Engineering|
|Depositing user:||Ms Katrina May|
|Date Deposited:||11 Feb 2010 14:18|
|Last modified:||22 May 2015 09:33|
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