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Linearized dynamical model for the nasa/ieee scole configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Collins, E. Hotz, A. F. Skelton, R. E. |
| Copyright Year | 1984 |
| Description | 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. |
| File Size | 752428 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840024353 |
| Archival Resource Key | ark:/13960/t9k40mx3x |
| Language | English |
| Publisher Date | 1984-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Euler-lagrange Equation Flexible Spacecraft Kinematics Spacecraft Control Dynamic Models Mathematical Models Control Theory Spacecraft Antennas Equations of Motion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
