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Derivation of generic error models procedure for 6-DOF motion system using multi-body kinematics

  • Yao Yu*
  • , Qu Zhiyong
  • *Corresponding author for this work
  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

6-DOF motion system capabilities on the field of simulation are becoming increasingly common. Regardless of the variety of kinematic configurations and structures, a kinematic model of the motion system has to be developed in order to determine the translational and rotational joint movements required to achieve a specified position and orientation of the missile relative to the point simulated. A generic and unified model is developed in this study as a viable alternative to the particular solutions that are only applicable to individual system configurations. Based on multi-body kinematics, each axis of the 6-DOF motion system is modeled using homogeneous coordinate transformation and small angle approximation. By synthesizing the system's parametric errors, an approach to model the effects of the positioning errors of a system's axes on the accuracy of the missile in its work space is developed. The developed versatile model makes the 6-DOF motion system model manageable and understandable.

Original languageEnglish
Title of host publication1st International Symposium on Systems and Control in Aerospace and Astronautics
Pages1267-1272
Number of pages6
StatePublished - 2006
Event1st International Symposium on Systems and Control in Aerospace and Astronautics - Harbin, China
Duration: 19 Jan 200621 Jan 2006

Publication series

Name1st International Symposium on Systems and Control in Aerospace and Astronautics
Volume2006

Conference

Conference1st International Symposium on Systems and Control in Aerospace and Astronautics
Country/TerritoryChina
CityHarbin
Period19/01/0621/01/06

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