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) |
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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