NASA Ames Research Center pilot George E. Tucker evaluates perspective flight guidance displays being developed by a Boeing/Ames research team for "runway independent aircraft." (Image courtesy of NASA
The course deals with introduction to design of feedback control systems, properties and advantages of feedback systems, time-domain and frequency-domain performance measures, stability and degree of stability. It also covers root locus method, nyquist criterion, frequency-domain design, and state space methods.
*Some translations represent previous versions of courses.