Robust autopilot design using μ-synthesis
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This paper examines the applicability of H∞ and μ-synthesis control to the design of automatic flight control systems for highly maneuverable, tail-controlled missiles. The impact on performance, of the degree of conservatism inherent to each approach, is examined. It is shown that μ-synthesis provides a superior framework for the design of missile autopilots which exhibit robust performance.
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