Operational Envelope of a Spatial Stewart Platform

[+] Author and Article Information
F. A. Adkins

Department of Applied Mathematical and Computational Sciences, University of Iowa, Iowa City, IA 52242

E. J. Haug

Department of Mechanical Engineering, University of Iowa, Iowa City, IA 52242

J. Mech. Des 119(2), 330-332 (Jun 01, 1997) (3 pages) doi:10.1115/1.2826256 History: Received June 01, 1996; Revised November 01, 1996; Online December 11, 2007


This technical brief presents the operational envelope for the spatial Stewart platform and dome of a six degree of freedom driving simulator, extending prior work that has been limited to planar mechanisms and manipulators. The set of all points in space that can be occupied by any point in the dome of the simulator is defined as its operational envelope. The geometry of the driving simulator’s dome and unilateral constraints on actuator lengths are incorporated and details of the defining equations for the operational envelope are given. Numerical methods are used to calculate the boundary of the operational envelope and results are presented in graphical form.

Copyright © 1997 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In