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Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical Report

机译:直升机飞行器实用最优飞行控制系统设计。第1卷:技术报告

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摘要

A method by which modern and classical theory techniques may be integrated in a synergistic fashion and used in the design of practical flight control systems is presented. A general procedure is developed, and several illustrative examples are included. Emphasis is placed not only on the synthesis of the design, but on the assessment of the results as well.

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