DocumentCode
3366906
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
fYear
2010
fDate
26-28 June 2010
Firstpage
6118
Lastpage
6122
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location
Wuhan, China
Print_ISBN
978-1-4244-7737-1
Type
conf
DOI
10.1109/MACE.2010.5536651
Filename
5536651
Link To Document