### Abstract

The optimal control problem of a spacecraft using continuous thrust where the terminal state and time interval are explicitly given is considered. We consider a new robust controller to the spacecraft rendezvous problem. Optimal rendezvous problem using continuous low-thrust is treated as optimal control problem and H_{∞} control. Using the property that both problems can be treated as two-point boundary value problem (TPVBP) of Hamiltonian system, we formulate the linear quadratic control with worst case disturbance rejection and worst case initial condition related by generating functions. Numerical simulations are given to illustrate the theory.

Original language | English |
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Title of host publication | Proceedings of SICE Annual Conference 2010, SICE 2010 - Final Program and Papers |

Publisher | Society of Instrument and Control Engineers (SICE) |

Pages | 804-810 |

Number of pages | 7 |

ISBN (Print) | 9784907764364 |

Publication status | Published - Jan 1 2010 |

Externally published | Yes |

### Publication series

Name | Proceedings of the SICE Annual Conference |
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### Fingerprint

### All Science Journal Classification (ASJC) codes

- Control and Systems Engineering
- Computer Science Applications
- Electrical and Electronic Engineering

### Cite this

*Proceedings of SICE Annual Conference 2010, SICE 2010 - Final Program and Papers*(pp. 804-810). [5603000] (Proceedings of the SICE Annual Conference). Society of Instrument and Control Engineers (SICE).