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

J Roberts, Peter Roberts

    Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-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 languageEnglish
    Title of host publicationAdvances in the Astronautical Sciences Vol. 119
    PublisherAmerican Astronautical Society
    Pages913-934
    Number of pages22
    Publication statusPublished - 31 Oct 2004
    Event14th AAS/AIAA Space Flight Mechanics Meeting Volume: Advances in the Astronautical Sciences Vol. 119 - Maui, Hawai'i
    Duration: 1 Feb 2004 → …

    Conference

    Conference14th AAS/AIAA Space Flight Mechanics Meeting Volume: Advances in the Astronautical Sciences Vol. 119
    CityMaui, Hawai'i
    Period1/02/04 → …

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