سال انتشار: ۱۳۸۶

محل انتشار: هفتمین همایش انجمن هوافضای ایران

تعداد صفحات: ۴

نویسنده(ها):

Majid Moavenian – Assistant Professor, Solid Mechanic Engineering Group, Mechanical Engineering Department, Ferdowsi University, Mashhad
Mohammad Reza Gharib – MSc Student, Solid Mechanic Engineering Group, Mechanical Engineering Department, Ferdowsi University, Mashhad
Mehdi Shahab – MSc Student, Solid Mechanic Engineering Group, Mechanical Engineering Department, Ferdowsi University, Mashhad

چکیده:

Quantitative design of robust control systems proposes a transparent and practical controller design methodology for uncertain single-input single-output and multivariable plants. There are several steps involved in the design of such controllers. The main steps involved in the design are template generation, loop shaping and pre-filter design. In this paper, a useful method to design a robust controller for yaw channel of a missile, using quantitative feedback theory (QFT) is proposed. Results are used to show the effectiveness of the proposed method.