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) |
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Pages (from-to) | 3307-3311 |
Number of pages | 5 |
Journal | Proceedings of the American Control Conference |
Volume | 5 |
State | Published - 1999 |
Externally published | Yes |
Event | Proceedings of the 1999 American Control Conference (99ACC) - San Diego, CA, USA Duration: Jun 2 1999 → Jun 4 1999 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering