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Modular design attitude control system (Document No: 19850001791)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chichester, F. D. |
| Copyright Year | 1984 |
| Description | A sequence of single axismodels and a series of reduced state linear observers of minimum order are used to reconstruct inaccessible variables pertaining to the modular attitude control of a rigid body flexible suspension model of a flexible spacecraft. The single axis models consist of two, three, four, and five rigid bodies, each interconnected by a flexible shaft passing through the mass centers of the bodies. Modal damping is added to each model. Reduced state linear observers are developed for synthesizing the inaccessible modal state variables for each modal model. |
| File Size | 3902433 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850001791 |
| Archival Resource Key | ark:/13960/t2z36np62 |
| Language | English |
| Publisher Date | 1984-10-05 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Linear Systems Torque Attitude Control Vibration Damping Flexible Spacecraft Problem Solving Scalars Mathematical Models Linear Equations Matrices Mathematics 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 |
