NASA NTRS · 19840024353
Linearized dynamical model for the NASA/IEEE SCOLE configuration
Abstract
The linearized equation of motion for the NASA/IEEE SCOLE configuration are developed. The derivation is based on the method of Lagrange and the equations are assembled into matrix second order form.
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Hotz, A. F., Collins, E., Skelton, R. E.. 1984-09-01. Linearized dynamical model for the NASA/IEEE SCOLE configuration. https://ntrs.nasa.gov/citations/19840024353
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