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http://dx.doi.org/10.5302/J.ICROS.2002.8.8.633

Study on Missile Aerodynamic Characteristics with Three Loop Acceleration Autopilot Structure  

Kim, Yoon-Sik (Agency for Defense Development)
Kim, Seung-Hwan (Agency for Defense Development)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.8, no.8, 2002 , pp. 633-638 More about this Journal
Abstract
We study how the missile autopilot with three loop acceleration structure is related to the aerodynamic characteristics. First, the relationships between the response characteristics of wingless-tail controlled missile and aerodynamics are derived. Next the maximum allowable performance limit of autopilot and the design direction for a missile shape are indicated using the property of zero. The method proposed in this paper may give a help to the missile autopilot system design and determination of the shape of aerodynamic. Also, the validity of proposed method is demonstrated via numerical example.
Keywords
three loop autopilot; aerodynamic characteristics; zero properties; wingless-tail control missile;
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  • Reference
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