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|
|Number of pages||8|
|State||Published - 1986|
ASJC Scopus subject areas
- Control and Systems Engineering