DocumentCode :
3554296
Title :
Analysis and implementation of a 6 DOF Steward platform-based force sensor for passive compliant robotic assembly
Author :
Nguyen, Charles C. ; Antrazi, Sami S. ; Zhou, Zhen-Lei
Author_Institution :
Dept. of Electr. Eng., Catholic Univ. of America, Washington, DC, USA
fYear :
1991
fDate :
7-10 Apr 1991
Firstpage :
880
Abstract :
The kinematic analysis of a 6-DOF (six-degree-of-freedom) force sensor whose design is based on the mechanism of the Stewart platform is presented. The force sensor is used to measure forces/torques and to provide passive compliance during part assembly. It is mainly composed of two platforms, the payload platform and the end-effector platform, coupled by six spring-loaded pistons whose length variations are measured by six linear voltage differential transformers mounted along the pistons. The forces and torques applied to the end-effector platform are computed by using the inverse and forward kinematic transformations of the Stewart platform, the known spring constants, and the piston length variations. Results of experiments conducted to evaluate the sensing capability of the force sensor used during the mating and demating of space-rated connectors are reported
Keywords :
aerospace control; assembling; electric sensing devices; force control; kinematics; microcomputer applications; robots; 6 DOF Steward platform-based force sensor; aerospace control; demating; end-effector platform; kinematic analysis; kinematic transformations; linear voltage differential transformers; mating; passive compliant robotic assembly; payload platform; sensing capability; space assembly; space-rated connectors; spring-loaded pistons; Assembly; Force measurement; Force sensors; Kinematics; Length measurement; Payloads; Pistons; Springs; Torque measurement; Transformers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Southeastcon '91., IEEE Proceedings of
Conference_Location :
Williamsburg, VA
Print_ISBN :
0-7803-0033-5
Type :
conf
DOI :
10.1109/SECON.1991.147886
Filename :
147886
Link To Document :
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