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Space station rotational equations of motion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rheinfurth, M. H. Carroll, S. N. |
| Copyright Year | 1985 |
| Description | Dynamic equations of motion are developed which describe the rotational motion for a large space structure having rotating appendages. The presence of the appendages produce torque coupling terms which are dependent on the inertia properties of the appendages and the rotational rates for both the space structure and the appendages. These equations were formulated to incorporate into the Space Station Attitude Control and Stabilization Test Bed to accurately describe the influence rotating solar arrays and thermal radiators have on the dynamic behavior of the Space Station. |
| File Size | 617893 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850025835 |
| Archival Resource Key | ark:/13960/t0wq4v85z |
| Language | English |
| Publisher Date | 1985-08-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Solar Arrays Attitude Control Stability Rotating Bodies Spacecraft Control Inertia Equations of Motion Space Station Structures Heat Radiators Space Stations Large Space Structures 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 |
