Spacecraft formation flying using bifurcating potential fields

Bennet, Derek and McInnes, Colin R. (2008) Spacecraft formation flying using bifurcating potential fields. In: 59th International Astronautical Congress, 2008-09-29 - 2008-10-03.

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Abstract

The distributed control of spacecraft flying in formation has been shown to have advantages over conventional single spacecraft systems. These include scalability, flexibility and robustness to failures. This paper considers the real problem of actuator saturation and shows how bound control laws can be developed that allow pattern formation and reconfigurability in a formation of spacecraft using bifurcating potential fields. In addition the stability of the system is ensured mathematically through dynamical systems theory.

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• Item metadata

  Item type:	Conference or Workshop Item(Paper)
  ID code:	7331
  Dates:	Date Event September 2008 Published
  Subjects:	Technology > Mechanical engineering and machinery Technology > Motor vehicles. Aeronautics. Astronautics
  Department:	Faculty of Engineering > Mechanical and Aerospace Engineering
  Depositing user:	Strathprints Administrator
  Date deposited:	08 Jan 2009 15:26
  Last modified:	09 Apr 2024 04:55
  Related URLs:	Journal or Publication Related item
  URI:	https://strathprints.strath.ac.uk/id/eprint/7331