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Study of the Effects of Discretizing Quantitative Feedback Theory Analog Control System Designs

机译:离散定量反馈理论模拟控制系统设计的效果研究

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This thesis examines the feasibility and a method of extending continuous domain Quantitative Feedback Theory (QFT) flight control system designs to the discrete domain. The results of two previous QFT analog design efforts are modified for a digital implementation. The first design effort is for the KC-135 transport aircraft. Robust analog fixed compensators are designed for three different flight conditions. The second design effort is for the AFTI/F-16 aircraft. In this design, parameter variation is due to both varying flight conditions and different aircraft configurations caused by failed surfaces. Keywords: Multivariable control.

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