Title :
Fuzzy controller for a PITOT-STATIC test set
Author :
Young, Christina M.
Author_Institution :
Smith Ind. Aerosp. & Defense Syst. Inc., Florham Park, NJ, USA
Abstract :
This paper describes a demonstration of fuzzy logic for a pneumatic control loop. The particular application examined is a ground-based aircraft pitot-static test set. This system is designed to achieve desired output pressures at given rates to simulate both airspeed (dynamic pressure) and altitude (static pressure). The design, development and performance of the fuzzy controller is examined and compared with a previously implemented proportional integral-differential (PID) controller
Keywords :
aerospace computer control; aircraft control; fuzzy control; fuzzy logic; knowledge based systems; pneumatic control equipment; pressure control; servomechanisms; PID controller; aircraft control; airspeed; altitude; dynamic pressure; fuzzy controller; fuzzy logic; ground-based aircraft; knowledge base; pitot-static test set; pneumatic control loop; static pressure; testing; training; Fuzzy control; Fuzzy sets; Jitter; Pneumatic systems; Pressure control; Servomechanisms; Testing; Thermodynamics; Transducers; Valves;
Conference_Titel :
Aerospace and Electronics Conference, 1993. NAECON 1993., Proceedings of the IEEE 1993 National
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-1295-3
DOI :
10.1109/NAECON.1993.290841
