Title :
Hydraulic system control logic for trunk line aircrafts
Author :
Jiang, HaoYi ; Ouyang, XiaoPing ; Yang, Huayong ; Lu Qing
Author_Institution :
State Key Lab. of Fluid Power Transm. & Control, Zhejiang Univ., Hangzhou, China
Abstract :
The background of designing hydraulic system control logic for trunk line aircraft was given. The hydraulic system scheme of trunk line aircrafts was introduced, including hydraulic system schematic, hydraulic users demand, system capacity, load shedding. A design method for control logic, status dividing-integrating, was proposed. And a design procedure, status analysis-signal definition-integrating-simulation validation, was introduced. Control logic system for hydraulic power system was designed and a simulation platform based on software was designed to validate control logic system designed.
Keywords :
Aerospace control; Aircraft; Control system synthesis; Control systems; Design methodology; Hydraulic systems; Logic design; Power system analysis computing; Power system control; Power system simulation; Aircraft; automatic control; hydraulic system; logic;
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location :
Wuhan, China
Print_ISBN :
978-1-4244-7737-1
DOI :
10.1109/MACE.2010.5536651
