Multivariable control of a twin lift helicopter system using the LQG/LTR design methodologyGuidelines for developing a multivariable centralized automatic flight control system (AFCS) for a twin lift helicopter system (TLHS) are presented. 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.
Document ID
19870026145
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rodriguez, A. A. (Massachusetts Inst. of Tech. Cambridge, MA, United States)