Design of flight control systems via robust decoupled servomechanism theoryDecoupling theory and robust servomechanism theory are applied to the design of linear multivariable systems with large parameter variations. In addition to being approximately decoupled in the transient period, the over-all system achieves tracking and disturbance rejection robustly in the steady state. An example in flight control system is given.
Document ID
19800040075
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Wang, S.-H. (Maryland, University College Park, Md., United States)
Davison, E. J. (Toronto, University Toronto, Canada)