Active formation along a circular orbit by pulse control

Mai Bando, Akira Ichikawa

研究成果: Contribution to conferencePaper査読

抄録

The relative motion of a follower satellite with respect to the leader in a given circular orbit is described by autonomous nonlinear differential equations. The linearized equations around the null solution are known as Hill- Clohessy-Wiltshire (HCW) equations. In this paper, active formation flying for the HCW system with pulse (impulse) control input is considered, where the desired relative orbit of the follower is generated by an exosystem. This allows for flexibility of the shape and period of the reference orbit. The output regulation theory for discrete linear system is employed. To show the effectiveness of this approach, numerical examples are given.

本文言語英語
ページ2197-2203
ページ数7
出版ステータス出版済み - 1 1 2013
イベント2013 52nd Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2013 - Nagoya, 日本
継続期間: 9 14 20139 17 2013

その他

その他2013 52nd Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2013
Country日本
CityNagoya
Period9/14/139/17/13

All Science Journal Classification (ASJC) codes

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

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