### Abstract

Formation flying along a halo orbit near the L_{1} point in the Sun-Earth circular restricted three-body system with impulse control is considered. The reference orbit is a periodic perturbation of the halo orbit generated by an exosystem, and the output regulation theory for discrete system is employed for the transition and maintenance. The minimum impulse number and the total velocity change required for the maintenance of the halo orbit are shown. Then the total velocity change for the maintenance of the perturbed reference orbits is shown. Finally, formation flying near the L_{1} point is considered, where the reference orbit is a periodic orbit whose frequency is equal to that of the linearized equations of motion at the L _{1} point.

Original language | English |
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Pages (from-to) | 3045-3057 |

Number of pages | 13 |

Journal | Unknown Journal |

Volume | 148 |

Publication status | Published - 2013 |

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### All Science Journal Classification (ASJC) codes

- Aerospace Engineering
- Space and Planetary Science

### Cite this

*Unknown Journal*,

*148*, 3045-3057.

**Flying near the libration points by impulse control.** / Bando, Mai; Ichikawa, Akira.

Research output: Contribution to journal › Article

*Unknown Journal*, vol. 148, pp. 3045-3057.

}

TY - JOUR

T1 - Flying near the libration points by impulse control

AU - Bando, Mai

AU - Ichikawa, Akira

PY - 2013

Y1 - 2013

N2 - Formation flying along a halo orbit near the L1 point in the Sun-Earth circular restricted three-body system with impulse control is considered. The reference orbit is a periodic perturbation of the halo orbit generated by an exosystem, and the output regulation theory for discrete system is employed for the transition and maintenance. The minimum impulse number and the total velocity change required for the maintenance of the halo orbit are shown. Then the total velocity change for the maintenance of the perturbed reference orbits is shown. Finally, formation flying near the L1 point is considered, where the reference orbit is a periodic orbit whose frequency is equal to that of the linearized equations of motion at the L 1 point.

AB - Formation flying along a halo orbit near the L1 point in the Sun-Earth circular restricted three-body system with impulse control is considered. The reference orbit is a periodic perturbation of the halo orbit generated by an exosystem, and the output regulation theory for discrete system is employed for the transition and maintenance. The minimum impulse number and the total velocity change required for the maintenance of the halo orbit are shown. Then the total velocity change for the maintenance of the perturbed reference orbits is shown. Finally, formation flying near the L1 point is considered, where the reference orbit is a periodic orbit whose frequency is equal to that of the linearized equations of motion at the L 1 point.

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M3 - Article

VL - 148

SP - 3045

EP - 3057

JO - Quaternary International

JF - Quaternary International

SN - 1040-6182

ER -