Abstract
We present the analysis of a nonlinear control system that is used to excite and maintain a specified amplitude of a lightly damped degree of freedom in the Jet Propulsion Laboratory microgyroscope. One- and two-degree-of-freedom models are considered. The analysis suggests that the perturbing effect of an additional weakly coupled degree of freedom does not quantitatively effect the operation of the automatic gain control.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 3307-3311 |
| Number of pages | 5 |
| Journal | Proceedings of the American Control Conference |
| Volume | 5 |
| State | Published - 1999 |
| Externally published | Yes |
ASJC Scopus subject areas
- Control and Systems Engineering