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Relative-Position Formation Control of Satellites using Electromagnetic Actuation with Piecewise-Sinusoidal Controls

Producción científica: Conference contributionrevisión exhaustiva

7 Citas (Scopus)

Resumen

We present a decentralized relative-position formation control algorithm for satellites with electromagnetic actuation. Each satellite's actuation system is driven by a sum of sinusoidal signals, each having different frequencies and piecewise constant amplitudes, which are considered as the controls. The piecewise-sinusoidal controls are designed to interact with neighbor satellites while decoupling interactions with non-neighbor satellites. Each satellite has relative-position and relative-velocity feedback of neighboring satellites, and the communication structure is a connected undirected graph. An ideal controller is designed based on an average dynamic model, and an optimal allocation scheme is used to compute the amplitude controls. The algorithm is demonstrated with a numerical example and a single-degree-of-freedom experiment.

Idioma originalEnglish
Título de la publicación alojada2020 American Control Conference, ACC 2020
Páginas4951-4956
Número de páginas6
ISBN (versión digital)9781538682661
DOI
EstadoPublished - jul 2020
Evento2020 American Control Conference, ACC 2020 - Denver, United States
Duración: jul 1 2020jul 3 2020

Serie de la publicación

NombreProceedings of the American Control Conference
Volumen2020-July
ISSN (versión impresa)0743-1619

Conference

Conference2020 American Control Conference, ACC 2020
País/TerritorioUnited States
CiudadDenver
Período7/1/207/3/20

Nota bibliográfica

Publisher Copyright:
© 2020 AACC.

Financiación

This work is supported by NASA under award 80NSSC17M0040 and NASA Kentucky under NASA award NNX15AR69H.

FinanciadoresNúmero del financiador
National Aeronautics and Space Administration80NSSC17M0040, NNX15AR69H

    ASJC Scopus subject areas

    • Electrical and Electronic Engineering

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