Model Verification of a Satellite with Large Flexible Appendages for Control System Design

Conference paper (2018)

Authors

E. Mooij Astrodynamics & Space Missions - Aerospace Engineering
D.I. Gransden Structural Integrity & Composites - Aerospace Engineering
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
Copyright: © 2018 E. Mooij, D.I. Gransden
DOI
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https://doi.org/10.2514/6.2018-0209
More Info
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Published Date

01-01-2018

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites

Abstract