A method for designing fixed-gain controllers and filters for systems with large parameter variation is presented. The approach is based on finding the minimax point of the Kullback information measure between the fixed-gain system and the optimal system at a given operating point. The effectiveness of the proposed approach is illustrated by designing a fixed-gain system for the short-period control of a high-performance aircraft and evaluating its performance over the flight envelope.
Information Approach to Fixed-Gain Design
IEEE Transactions on Aerospace and Electronic Systems ; AES-21 , 1 ; 47-55
1985-01-01
1582620 byte
Article (Journal)
Electronic Resource
English
Information approach to fixed-gain design (aircraft control)
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