PID and Fuzzy Logic Pitch Attitude Hold Systems for a Fighter Jet
AIAA Guidance, Navigation, and Control Conference and Exhibit
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2002-4646 PID and Fuzzy Logic Pitch Attitude Hold Systems for a Fighter Jet
British Library Conference Proceedings | 2002
|Design of Robust Quantitative Feedback Theory Controllers for Pitch Attitude Hold Systems
Online Contents | 1994
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