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Two different approaches for a control law of single gimbal control moment gyros
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schiehlen, W. O. |
| Copyright Year | 1972 |
| Description | In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCMG) are of increasing interest. A gimbal angle approach and a gimbal rate approach are presented for the SGCMG control law including the singularity avoidance. Both approaches are compared and some illustrative examples are given. |
| File Size | 1159419 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720024010 |
| Archival Resource Key | ark:/13960/t9j43hw13 |
| Language | English |
| Publisher Date | 1972-08-02 |
| Access Restriction | Open |
| Subject Keyword | Navigation Spacecraft Control Momentum Transfer Attitude Control Gimbals Control Moment Gyroscopes Angular Momentum Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |