### Abstract

Using two impulsive maneuvers of fixed magnitudes, transfers between two circular orbits are possible only for certain thrust directions. This paper develops the feasibility domain for the two impulses, and criteria for determining the thrust directions. Two theorems, concerning the number of possible final orbits that are circular and their radii, are proven. These are applied to an example optimization problem involving a minimum change in orbital radius during the transfer.

Original language | English (US) |
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Title of host publication | Advances in the Astronautical Sciences |

Pages | 833-842 |

Number of pages | 10 |

Volume | 75 |

Edition | pt 2 |

State | Published - 1991 |

Event | Proceedings of the AAS/AIAA Spaceflight Mechanics Meeting Part 2 (of 2) - Houston, TX, USA Duration: Feb 11 1991 → Feb 13 1991 |

### Other

Other | Proceedings of the AAS/AIAA Spaceflight Mechanics Meeting Part 2 (of 2) |
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City | Houston, TX, USA |

Period | 2/11/91 → 2/13/91 |

### Fingerprint

### All Science Journal Classification (ASJC) codes

- Aerospace Engineering

### Cite this

*Advances in the Astronautical Sciences*(pt 2 ed., Vol. 75, pp. 833-842)

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*Advances in the Astronautical Sciences.*pt 2 edn, vol. 75, pp. 833-842, Proceedings of the AAS/AIAA Spaceflight Mechanics Meeting Part 2 (of 2), Houston, TX, USA, 2/11/91.

**Transfers between circular orbits using fixed impulses.** / Jin, Houzhi; Melton, Robert Graham.

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

TY - GEN

T1 - Transfers between circular orbits using fixed impulses

AU - Jin, Houzhi

AU - Melton, Robert Graham

PY - 1991

Y1 - 1991

N2 - Using two impulsive maneuvers of fixed magnitudes, transfers between two circular orbits are possible only for certain thrust directions. This paper develops the feasibility domain for the two impulses, and criteria for determining the thrust directions. Two theorems, concerning the number of possible final orbits that are circular and their radii, are proven. These are applied to an example optimization problem involving a minimum change in orbital radius during the transfer.

AB - Using two impulsive maneuvers of fixed magnitudes, transfers between two circular orbits are possible only for certain thrust directions. This paper develops the feasibility domain for the two impulses, and criteria for determining the thrust directions. Two theorems, concerning the number of possible final orbits that are circular and their radii, are proven. These are applied to an example optimization problem involving a minimum change in orbital radius during the transfer.

UR - http://www.scopus.com/inward/record.url?scp=0025724379&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0025724379&partnerID=8YFLogxK

M3 - Conference contribution

SN - 0877033390

VL - 75

SP - 833

EP - 842

BT - Advances in the Astronautical Sciences

ER -