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.
|Title of host publication
|Proceedings of the American Control Conference
|Number of pages
|Published - 1986
ASJC Scopus subject areas
- Control and Systems Engineering