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This paper presents some of the fundamental principles involved in missile autopilot design using the well known classical control approaches and allows a guidance engineer to grasp a sound understanding and knowledge in this field. In addition, the paper provides a robust classic controller for stabilizing the guidance system of a beam rider guided missile in addition to satisfying the performance requirements upon miss distance and demanded normal acceleration. The paper presents the analysisdoi:10.21608/iceeng.1998.61097 fatcat:iy57ry43jnfljfyglep5cv4bpu