### Abstract

hybrid of solar sail and a solar electric propulsion (SEP). A feedback linearization

control scheme is implemented to perform stabilization and trajectory tracking for

the nonlinear system. Attention is now directed to binary asteroid systems as an

application of the restricted problem. The idea of combining a solar sail with an

SEP auxiliary system to obtain a hybrid sail system is important especially due to

the challenges of performing complex trajectories.

Language | English |
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Pages | Article AAS12-130 |

Number of pages | 16 |

Publication status | Published - 29 Jan 2012 |

Event | 22nd AAS/AIAA Spaceflight Mechanics Meeting - Charleston, South Carolina, United States Duration: 29 Jan 2012 → 2 Feb 2012 |

### Conference

Conference | 22nd AAS/AIAA Spaceflight Mechanics Meeting |
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Country | United States |

City | Charleston, South Carolina |

Period | 29/01/12 → 2/02/12 |

### Fingerprint

### Keywords

- periodic orbits
- circular restricted Earth-Moon system (CRTBP)
- solar electric propulsion (SEP)
- solar sail
- trajectory tracking
- binary asteroid systems
- hybrid sail system

### Cite this

*Feedback stabilization of displaced periodic orbits: Application to binary asteroid*. Article AAS12-130. Paper presented at 22nd AAS/AIAA Spaceflight Mechanics Meeting, Charleston, South Carolina, United States.

}

**Feedback stabilization of displaced periodic orbits : Application to binary asteroid.** / Simo, Jules; McInnes, Colin.

Research output: Contribution to conference › Paper

TY - CONF

T1 - Feedback stabilization of displaced periodic orbits

T2 - Application to binary asteroid

AU - Simo, Jules

AU - McInnes, Colin

PY - 2012/1/29

Y1 - 2012/1/29

N2 - This paper investigates displaced periodic orbits at linear order in the circular restricted Earth-Moon system (CRTBP), where the third massless body utilizes ahybrid of solar sail and a solar electric propulsion (SEP). A feedback linearizationcontrol scheme is implemented to perform stabilization and trajectory tracking forthe nonlinear system. Attention is now directed to binary asteroid systems as anapplication of the restricted problem. The idea of combining a solar sail with anSEP auxiliary system to obtain a hybrid sail system is important especially due tothe challenges of performing complex trajectories.

AB - This paper investigates displaced periodic orbits at linear order in the circular restricted Earth-Moon system (CRTBP), where the third massless body utilizes ahybrid of solar sail and a solar electric propulsion (SEP). A feedback linearizationcontrol scheme is implemented to perform stabilization and trajectory tracking forthe nonlinear system. Attention is now directed to binary asteroid systems as anapplication of the restricted problem. The idea of combining a solar sail with anSEP auxiliary system to obtain a hybrid sail system is important especially due tothe challenges of performing complex trajectories.

KW - periodic orbits

KW - circular restricted Earth-Moon system (CRTBP)

KW - solar electric propulsion (SEP)

KW - solar sail

KW - trajectory tracking

KW - binary asteroid systems

KW - hybrid sail system

UR - http://www.space-flight.org/docs/2012_winter/final_program.pdf

M3 - Paper

SP - Article AAS12-130

ER -