### Abstract

The focus of this paper is to present a preliminary study concerning relative motion and rendezvous in the restricted three-body problem. This paper presents full numerical simulations compared with linearized results of relative motion around well-known Lagrangian orbits such as halo orbits around Earth-Moon L2. Additionally, an initial linearization study is performed and presented to understand the general dynamics of such relative motion. Previous work on this topic relies on simplifications and assumptions that constrain the results to specific spatial domains and geometries. The reason to analyze such motion in linearized form as opposed to purely numerically integrate the equations of motion is to being able to study rendezvous and formation flying maneuvers around multiple families of Lagrangian orbits at once. Additionally, analytical and linearized analyses can provide important physical insight and help to quickly determine optimal solutions when searching through a large tradespace of orbital transfers and rendezvous maneuvers for both control-free and controlled dynamics. Future work is aimed to develop algorithms that, given a nominal Lagrangian orbit of interest, can describe the relative motion of two spacecraft that are operating "close" to each. Thus a more streamlined analytical work will be developed to compute which maneuvers are optimal to reduce Δv consumption, time of flight, or other parameters of interest.

Original language | English (US) |
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Title of host publication | Spaceflight Mechanics 2016 |

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

Publisher | Univelt Inc. |

Pages | 4445-4463 |

Number of pages | 19 |

ISBN (Print) | 9780877036333 |

State | Published - Jan 1 2016 |

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

### Publication series

Name | Advances in the Astronautical Sciences |
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Volume | 158 |

ISSN (Print) | 0065-3438 |

### Other

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

City | Napa |

Period | 2/14/16 → 2/18/16 |

### Fingerprint

### All Science Journal Classification (ASJC) codes

- Aerospace Engineering
- Space and Planetary Science

### Cite this

*Spaceflight Mechanics 2016*(pp. 4445-4463). (Advances in the Astronautical Sciences; Vol. 158). Univelt Inc..

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*Spaceflight Mechanics 2016.*Advances in the Astronautical Sciences, vol. 158, Univelt Inc., pp. 4445-4463, 26th AAS/AIAA Space Flight Mechanics Meeting, 2016, Napa, United States, 2/14/16.

**Preliminary study on relative motion and rendezvous between spacecraft in the restricted three-body problem.** / Conte, Davide; Spencer, David B.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

TY - GEN

T1 - Preliminary study on relative motion and rendezvous between spacecraft in the restricted three-body problem

AU - Conte, Davide

AU - Spencer, David B.

PY - 2016/1/1

Y1 - 2016/1/1

N2 - The focus of this paper is to present a preliminary study concerning relative motion and rendezvous in the restricted three-body problem. This paper presents full numerical simulations compared with linearized results of relative motion around well-known Lagrangian orbits such as halo orbits around Earth-Moon L2. Additionally, an initial linearization study is performed and presented to understand the general dynamics of such relative motion. Previous work on this topic relies on simplifications and assumptions that constrain the results to specific spatial domains and geometries. The reason to analyze such motion in linearized form as opposed to purely numerically integrate the equations of motion is to being able to study rendezvous and formation flying maneuvers around multiple families of Lagrangian orbits at once. Additionally, analytical and linearized analyses can provide important physical insight and help to quickly determine optimal solutions when searching through a large tradespace of orbital transfers and rendezvous maneuvers for both control-free and controlled dynamics. Future work is aimed to develop algorithms that, given a nominal Lagrangian orbit of interest, can describe the relative motion of two spacecraft that are operating "close" to each. Thus a more streamlined analytical work will be developed to compute which maneuvers are optimal to reduce Δv consumption, time of flight, or other parameters of interest.

AB - The focus of this paper is to present a preliminary study concerning relative motion and rendezvous in the restricted three-body problem. This paper presents full numerical simulations compared with linearized results of relative motion around well-known Lagrangian orbits such as halo orbits around Earth-Moon L2. Additionally, an initial linearization study is performed and presented to understand the general dynamics of such relative motion. Previous work on this topic relies on simplifications and assumptions that constrain the results to specific spatial domains and geometries. The reason to analyze such motion in linearized form as opposed to purely numerically integrate the equations of motion is to being able to study rendezvous and formation flying maneuvers around multiple families of Lagrangian orbits at once. Additionally, analytical and linearized analyses can provide important physical insight and help to quickly determine optimal solutions when searching through a large tradespace of orbital transfers and rendezvous maneuvers for both control-free and controlled dynamics. Future work is aimed to develop algorithms that, given a nominal Lagrangian orbit of interest, can describe the relative motion of two spacecraft that are operating "close" to each. Thus a more streamlined analytical work will be developed to compute which maneuvers are optimal to reduce Δv consumption, time of flight, or other parameters of interest.

UR - http://www.scopus.com/inward/record.url?scp=85007306961&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85007306961&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:85007306961

SN - 9780877036333

T3 - Advances in the Astronautical Sciences

SP - 4445

EP - 4463

BT - Spaceflight Mechanics 2016

A2 - Ozimek, Martin T.

A2 - Zanetti, Renato

A2 - Bowes, Angela L.

A2 - Russell, Ryan P.

A2 - Ozimek, Martin T.

PB - Univelt Inc.

ER -