A simplified computational method for two-body high spinning rate vehicles-Reference-Cited by-同舟云学术

A simplified computational method for two-body high spinning rate vehicles

Published:2020-10 Issue: Volume:105 Page:106050
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

de Celis Raúl^ORCID,Cadarso Luis,Fuentes Manuel^ORCID

Funder

“Dirección General de Investigación e Innovación Tecnológica, Consejería de Ciencia, Universidades e Innovación, Comunidad de Madrid” and “Universidad Rey Juan Carlos”

Publisher

Elsevier BV

Subject

Aerospace Engineering

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5. Attitude guidance for spinning vehicles with independent pitch and yaw control;Creagh;J. Guid. Control Dyn.,2010

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