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Copyright © 2003 Marcel Dekker, Inc. Introduction 11 student who is an F-16 pilot . He was able to utilize his realworld knowledge of the aircraft and its handling qualities to achieve the desired robust FCS. Traditionally, flight control engineers have taken a conservative, brute force approach to designing a full envelope FCS for an aircraft. First, many design points, which for this design were points representing airspeed vs. altitude, within and along the border of the flight envelope plot were selected.
For proper operation the power level of the reactor must be maintained at a desired value or must vary in a prescribed manner. This must be accomplished automatically with minimum human supervision. 13 is a simplified block diagram of a feedback control system for controlling the power output level of a reactor. If the power output level differs Copyright © 2003 Marcel Dekker, Inc. Introduction 17 Antiaircraft radar-tracking control systems. 12 from the reference input value, the actuating signal produces a signal at the output of the control elements.
9 OUTLINE OF TEXT The text is essentially divided into three parts. The first part, consisting of Chapters 2 through 4, provides the mathematical foundation for modeling physical systems and obtaining time solutions using classical or Laplace transform methods. The remaining portion of the text represents material that is usually covered in the first or second undergraduate course in control theory and control system design. The first few chapters deal with the mathematics and physical system modeling that underlie the analysis of control systems.