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

Giorgio Mingotti, Francesco Topputo, Franco Bernelli-Zazzara

Research output: Chapter in Book/Report/Conference proceedingChapter

1 Citation (Scopus)
LanguageEnglish
Title of host publicationSpaceflight Mechanics 2012
Pages541-556
Volume143
ISBN (Electronic)978-0-87703-581-7
Publication statusPublished - Feb 2012
Event22nd AAS/AIAA Spaceflight Mechanics Meeting - Charleston, South Carolina, United States
Duration: 29 Jan 20122 Feb 2012

Publication series

NameAdvances in the Astronautical Sciences
PublisherUnivelt Inc
No.1-3
Volume143
ISSN (Print)1081-6003

Conference

Conference22nd AAS/AIAA Spaceflight Mechanics Meeting
CountryUnited States
CityCharleston, South Carolina
Period29/01/122/02/12

Keywords

  • restricted 3-body problem
  • Earth-Moon trajectories
  • low-energy
  • periodic orbits
  • transit orbits
  • transfers
  • optimisation
  • capture
  • system
  • Mars

Cite this

Mingotti, G., Topputo, F., & Bernelli-Zazzara, F. (2012). Attainable sets in space mission design: A method to define low-thrust, invariant manifold trajectories. In Spaceflight Mechanics 2012 (Vol. 143, pp. 541-556). (Advances in the Astronautical Sciences; Vol. 143, No. 1-3).
Mingotti, Giorgio ; Topputo, Francesco ; Bernelli-Zazzara, Franco. / Attainable sets in space mission design : A method to define low-thrust, invariant manifold trajectories. Spaceflight Mechanics 2012. Vol. 143 2012. pp. 541-556 (Advances in the Astronautical Sciences; 1-3).
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Mingotti, G, Topputo, F & Bernelli-Zazzara, F 2012, Attainable sets in space mission design: A method to define low-thrust, invariant manifold trajectories. in Spaceflight Mechanics 2012. vol. 143, Advances in the Astronautical Sciences, no. 1-3, vol. 143, pp. 541-556, 22nd AAS/AIAA Spaceflight Mechanics Meeting, Charleston, South Carolina, United States, 29/01/12.

Attainable sets in space mission design : A method to define low-thrust, invariant manifold trajectories. / Mingotti, Giorgio; Topputo, Francesco; Bernelli-Zazzara, Franco.

Spaceflight Mechanics 2012. Vol. 143 2012. p. 541-556 (Advances in the Astronautical Sciences; Vol. 143, No. 1-3).

Research output: Chapter in Book/Report/Conference proceedingChapter

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T1 - Attainable sets in space mission design

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AU - Mingotti, Giorgio

AU - Topputo, Francesco

AU - Bernelli-Zazzara, Franco

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KW - Earth-Moon trajectories

KW - low-energy

KW - periodic orbits

KW - transit orbits

KW - transfers

KW - optimisation

KW - capture

KW - system

KW - Mars

UR - http://www.amazon.com/Spaceflight-Mechanics-Advances-Astronautical-Sciences/dp/0877035814

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BT - Spaceflight Mechanics 2012

ER -

Mingotti G, Topputo F, Bernelli-Zazzara F. Attainable sets in space mission design: A method to define low-thrust, invariant manifold trajectories. In Spaceflight Mechanics 2012. Vol. 143. 2012. p. 541-556. (Advances in the Astronautical Sciences; 1-3).