Attainable sets in space mission design : A method to define low-thrust, invariant manifold trajectories

Mingotti, Giorgio and Topputo, Francesco and Bernelli-Zazzara, Franco; (2012) Attainable sets in space mission design : A method to define low-thrust, invariant manifold trajectories. In: Spaceflight Mechanics 2012. Advances in the Astronautical Sciences, 143 . Univelt Inc, USA, pp. 541-556. ISBN 978-0-87703-581-7

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• Item metadata

  Item type:	Book Section
  ID code:	46904
  Dates:	Date Event February 2012 Published
  Keywords:	restricted 3-body problem, Earth-Moon trajectories, low-energy, periodic orbits, transit orbits, transfers, optimisation, capture, system, Mars, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Mechanical Engineering, Aerospace Engineering, Control and Systems Engineering, Space and Planetary Science
  Subjects:	Technology > Mechanical engineering and machinery Technology > Motor vehicles. Aeronautics. Astronautics
  Department:	Faculty of Engineering > Mechanical and Aerospace Engineering
  Depositing user:	Pure Administrator
  Date deposited:	26 Feb 2014 11:32
  Last modified:	26 Mar 2023 01:51
  Related URLs:	Related item
  URI:	https://strathprints.strath.ac.uk/id/eprint/46904