DocumentCode
2338463
Title
Initial disturbance accommodating control system analysis for prototype electromechanical Space Shuttle steering actuator
Author
Wander, John ; Byrd, Virginia ; Parker, Joey
Author_Institution
Dept. of Mech. Eng., Alabama Univ., Tuscaloosa, AL, USA
Volume
6
fYear
1995
fDate
21-23 Jun 1995
Firstpage
3961
Abstract
A comparison of model responses between the existing hydraulic actuator used to steer the Space Shuttle and a prototype actuator indicate that active force control is needed with the prototype. The prototype is based on electric motor actuation and roller screw transmission
Keywords
actuators; aerospace control; control system analysis; electric actuators; space vehicles; stability; active force control; electric motor actuation; hydraulic actuator; initial disturbance accommodating control system analysis; model responses; prototype electromechanical Space Shuttle steering actuator; roller screw transmission; Control system analysis; Engine cylinders; Fasteners; Hydraulic actuators; NASA; Prototypes; Resonance; Space shuttles; Springs; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, Proceedings of the 1995
Conference_Location
Seattle, WA
Print_ISBN
0-7803-2445-5
Type
conf
DOI
10.1109/ACC.1995.532675
Filename
532675
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