## Abstract

The paper presents an approach to the design of an optimal collision avoidance maneuver under model uncertainty. The dynamical model is assumed to be only partially known and the missing components are modeled with a polynomial expansion whose coefficients are recovered from sparse observations. The resulting optimal control problem is then translated into a robust reachability problem in which a controlled object has to avoid the region of possible collisions, in a given time, with a given target.

The paper will present a solution for a circular orbit in the case in which the reachable set is given by the level set of an artificial potential function.

The paper will present a solution for a circular orbit in the case in which the reachable set is given by the level set of an artificial potential function.

Original language | English |
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Title of host publication | Spaceflight Mechanics 2016 |

Editors | Renato Zanetti, Ryan P. Russell, Martin T. Ozimek, Angela L. Bowes |

Pages | 4049-4064 |

Number of pages | 16 |

Volume | 158 |

Publication status | Published - 14 Feb 2016 |

Event | 26th AAS/AIAA Space Flight Mechanics Meeting, 2016 - Napa, United States Duration: 14 Feb 2016 → 18 Feb 2016 |

### Conference

Conference | 26th AAS/AIAA Space Flight Mechanics Meeting, 2016 |
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Country | United States |

City | Napa |

Period | 14/02/16 → 18/02/16 |

## Keywords

- collision avoidance
- circular orbit
- near earth object