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A Flexible Appendage Model for Use in Integrated Control/Structure Spacecraft Design

Perez Gonzalez, José Alvaro and Pittet, Christelle and Alazard, Daniel and Loquen, Thomas and Cumer, Christelle A Flexible Appendage Model for Use in Integrated Control/Structure Spacecraft Design. (2015) In: 1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles (ACNAAV’15), 10 June 2015 - 12 June 2015 (Séville, Spain).

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Official URL: http://dx.doi.org/10.1016/j.ifacol.2015.08.096

Abstract

The study presents and validates a flexible appendage model to be used in an integrated control/structure spacecraft design. The integrated design methodology needs an accurate LFT representation of spacecraft flexible appendages so that parametric variations can be included. This requirement can be met using the Interconnected Flexible Appendage model studied in Perez et al. (2015). The model suitability is validated through the modeling of a real deployable boom, obtaining the same frequency modes and dynamical behavior.

Item Type:Conference or Workshop Item (Paper)
HAL Id:hal-01413395
Audience (journal):International peer-reviewed journal
Audience (conference):International conference proceedings
Uncontrolled Keywords:
Institution:French research institutions > Centre National d'Études Spatiales - CNES (FRANCE)
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE)
French research institutions > Office National d'Etudes et Recherches Aérospatiales - ONERA (FRANCE)
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Deposited By: Daniel Alazard
Deposited On:09 Dec 2016 16:00

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