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
fDate :
29 June-1 July 1994
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;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.752489
