Interplanetary trajectory design of solar sail spacecraft utilizing an invariant manifold

Yutaro Ishida, Shinji Hokamoto

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper deals with an in-plane trajectory design method for a solar sail spacecraft to rendezvous with a planet. In the interplanetary rendezvous problem, the spacecraft's velocity must coincide with the orbital velocity of the planet when it reaches the planet's orbit. This paper proposes a trajectory design procedure that utilizes an invariant manifold for a specified control profile to reach a target orbit. The proposed strategy allows a rendezvous to a planet in an elliptical orbit by adjusting the launch timing of the sailcraft when it starts from a circular orbit. Numerical simulations demonstrate the validity of the proposed procedure.

Original languageEnglish
Title of host publicationAIAA/AAS Astrodynamics Specialist Conference 2010
DOIs
Publication statusPublished - Dec 1 2010
EventAIAA/AAS Astrodynamics Specialist Conference 2010 - Toronto, ON, Canada
Duration: Aug 2 2010Aug 5 2010

Publication series

NameAIAA/AAS Astrodynamics Specialist Conference 2010

Other

OtherAIAA/AAS Astrodynamics Specialist Conference 2010
CountryCanada
CityToronto, ON
Period8/2/108/5/10

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Energy(all)

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  • Cite this

    Ishida, Y., & Hokamoto, S. (2010). Interplanetary trajectory design of solar sail spacecraft utilizing an invariant manifold. In AIAA/AAS Astrodynamics Specialist Conference 2010 (AIAA/AAS Astrodynamics Specialist Conference 2010). https://doi.org/10.2514/6.2010-8137