DocumentCode
281843
Title
The use of structured models for the simulation of pneumatic control systems
Author
Bradshaw, A. ; Counsell, J.M. ; Diggles, S.
Author_Institution
Lancaster Univ., UK
fYear
1989
fDate
32619
Firstpage
42370
Lastpage
42373
Abstract
In order to meet more demanding dynamic performance specifications for pneumatic control systems, designs are becoming increasingly complex and require precision tuning to achieve optimum performance over a wide range of operating conditions. These complex designs are normally a result of an extended development programme which has often required the incorporation of additional components of palliative solutions to problems identified during performance tests. These tests, carried out at great cost, rarely cover all operating conditions. Consequently, confidence in the design becomes low when operating conditions are not these which have already been considered in the test programme. These development costs can be curtailed by the intelligent use of properly developed and validated digital computer simulation models. In this paper it is shown how such models can be readily established using a structured, Fortran-based simulation language. Furthermore, it is shown how a series of submodels can be used to develop a simulation model of a gas servomechanism for missile control fin deflection
Keywords
aerospace control; aerospace simulation; control system CAD; digital simulation; missiles; pneumatic control equipment; pneumatic systems; servomechanisms; Fortran-based simulation language; complex designs; development costs; development programme; digital computer simulation models; dynamic performance specifications; gas servomechanism; missile control fin deflection; operating conditions; optimum performance; performance tests; pneumatic control systems; precision tuning; structured models; submodels;
fLanguage
English
Publisher
iet
Conference_Titel
CAD in the Aerospace Industry, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
198299
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