A Method for designing fixed gain controllers and filters for systems with large parameter variation is presented. The approach, based of minmax information criteria, is used to design a non-adaptive back-up control system for a given aircraft and is shown to provide good performance qualities. (Author)
Fixed Gain Controller Design for Aircraft
1981
31 pages
Report
No indication
English
Avionics , Flight control systems , Control theory , Optimization , Gain , Filters , Dynamic response , Computer applications , Minimax technique , Information theory , Estimates , Variations , Stochastic processes , Backup systems , Adaptive control systems , Foreign technology , Fixed gain controllers
Information approach to fixed-gain design (aircraft control)
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