Abstract
Guidelines are presented for developing a multivariable, centralized automatic flight control system for a twin lift helicopter system. Singular value ideas are used to formulate performance and stability robustness specifications. A linear-quadratic-Gaussian with loop-transfer-recovery (LQG/LTR) design is obtained and evaluated.
| Original language | English (US) |
|---|---|
| Title of host publication | Proceedings of the American Control Conference |
| Publisher | IEEE |
| Pages | 1325-1332 |
| Number of pages | 8 |
| State | Published - 1986 |
| Externally published | Yes |
ASJC Scopus subject areas
- Control and Systems Engineering