Spacecraft formation flying using bifurcating potential fields

Derek Bennet; Colin R. McInnes

Spacecraft formation flying using bifurcating potential fields

Derek Bennet, Colin R. McInnes

Mechanical And Aerospace Engineering

Research output: Contribution to conference › Paper › peer-review

15 Citations (Scopus)

83 Downloads (Pure)

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.

Original language	English
Number of pages	9
Publication status	Published - Sep 2008
Event	59th International Astronautical Congress - Glasgow, Scotland Duration: 29 Sep 2008 → 3 Oct 2008

Conference

Conference	59th International Astronautical Congress
City	Glasgow, Scotland
Period	29/09/08 → 3/10/08

Keywords

spacecraft
space travel
bifurcation
actuator saturation
dynamical systems theory

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strathprints007331Accepted author manuscript, 253 KB

Cite this

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title = "Spacecraft formation flying using bifurcating potential fields",

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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AU - Bennet, Derek

AU - McInnes, Colin R.

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N2 - 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.

AB - 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.

KW - spacecraft

KW - space travel

KW - bifurcation

KW - actuator saturation

KW - dynamical systems theory

UR - https://iafastro.directory/iac/archive/browse/IAC-08/

UR - https://iafastro.directory/iac/archive/browse/IAC-08/C1/6/1161/

M3 - Paper

T2 - 59th International Astronautical Congress

Y2 - 29 September 2008 through 3 October 2008

ER -

Spacecraft formation flying using bifurcating potential fields

Abstract

Conference

Keywords

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