The Development of High Fidelity linearised J2 Models for Satellite Formation Flying Control

J Roberts; Peter Roberts

The Development of High Fidelity linearised J2 Models for Satellite Formation Flying Control

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

Abstract

The inclusion of the linearized J 2 effect in the Hill equations of relative motion gives greater insight into satellite formation flying dynamics, and the opportunity to investigate alternative feedback control strategies for the station keeping task. Th

Original language	English
Title of host publication	Advances in the Astronautical Sciences Vol. 119
Publisher	American Astronautical Society
Pages	913-934
Number of pages	22
Publication status	Published - 31 Oct 2004
Event	14th AAS/AIAA Space Flight Mechanics Meeting Volume: Advances in the Astronautical Sciences Vol. 119 - Maui, Hawai'i Duration: 1 Feb 2004 → …

Conference

Conference	14th AAS/AIAA Space Flight Mechanics Meeting Volume: Advances in the Astronautical Sciences Vol. 119
City	Maui, Hawai'i
Period	1/02/04 → …

Cite this

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title = "The Development of High Fidelity linearised J2 Models for Satellite Formation Flying Control",

abstract = "The inclusion of the linearized J 2 effect in the Hill equations of relative motion gives greater insight into satellite formation flying dynamics, and the opportunity to investigate alternative feedback control strategies for the station keeping task. Th",

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AB - The inclusion of the linearized J 2 effect in the Hill equations of relative motion gives greater insight into satellite formation flying dynamics, and the opportunity to investigate alternative feedback control strategies for the station keeping task. Th

M3 - Conference contribution

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T2 - 14th AAS/AIAA Space Flight Mechanics Meeting Volume: Advances in the Astronautical Sciences Vol. 119

Y2 - 1 February 2004

ER -

The Development of High Fidelity linearised J2 Models for Satellite Formation Flying Control

Abstract

Conference

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