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Fundamentals of Flight Vehicle Control (3521)

Description

  • Linear dynamic systems analysis using Transfer function (Laplace Transformation based) methods and State Space (matrix theory based) methods with emphasis on aircraft and spacecraft models. Prereq: 3520 (520) and ECE 2300 (300 and 309), and enrollment as AeroEng-BS student (No pre-majors can enroll in this class). Not open to students with credit for 521. Units: 3 credit hours.

Subject

  • Aeronautical and Astro Engr (AEROENG)