Title :
Study on Flow Matching Intelligent Control for Aircraft Pressure Refueling Management System
Author :
Cao, Keqiang ; Hu, Liangmou
Author_Institution :
Eng. Inst., Air Force Eng. Univ., Xi´´an
Abstract :
A new method for performance optimization of aircraft pressure refueling management system is presented. The refueling time model of the system is established, and the optimum design goal is set up. Alterable throttles are put forward to achieve the goal of flow matching, and intelligent PID controller is presented to regulate the real-time flow of every pipeline. The simulation results show that single nerve cell adaptive PID controller, especially improved single nerve cell adaptive PID controller, has characteristics of simple algorithms, strong real time and robustness, which can meet the control demands for aircraft pressure refueling management system. The results of ground simulated test show that it is feasible and valid
Keywords :
adaptive control; aircraft control; fuel systems; intelligent control; optimisation; three-term control; aircraft pressure refueling management system; flow matching intelligent control; performance optimization; refueling time model; single nerve cell adaptive PID controller; throttle; Adaptive control; Aerospace control; Aircraft; Intelligent control; Optimization; Pipelines; Pressure control; Programmable control; Real time systems; Three-term control; flow matching; intelligent PID control; pressure refueling; refueling time; throttle;
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
DOI :
10.1109/WCICA.2006.1713494