DocumentCode
335519
Title
Dynamic controller design for a fixed base motion simulator
Author
Repperger, D.W. ; Huang, Ming Z. ; Roberts, R.G.
Author_Institution
Armstrong Lab., Wright-Patterson AFB, OH, USA
Volume
2
fYear
1994
fDate
29 June-1 July 1994
Firstpage
2298
Abstract
Different PID controller designs are investigated for construction of a closed loop compensator to reduce tracking error. This technique is applied to a large motion simulator used to emulate supermaneuverable flight and modeled as a robotic system.
Keywords
aerospace simulation; aerospace test facilities; aircraft control; closed loop systems; three-term control; PID controller designs; closed-loop compensator; dynamic controller design; fixed-base motion simulator; robotic system; supermaneuverable flight; tracking error; Aerospace simulation; End effectors; Equations; Error correction; Laboratories; Lagrangian functions; Motion control; Solid modeling; Symmetric matrices; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.752489
Filename
752489
Link To Document