The amendatory method of three dimensional rotary mechanisms

DOI

10.2991/icmse-15.2015.67How to use a DOI?

Keywords

The Captive Trajectory Simulation, homogeneous transformation matrix, coordinative control.

Abstract

First, the author measures the pose of the aircraft model under the help of Laser Tracker System; then, the author creates the amendatory equation on the bases of measuring; At last, the compensation value is input into the control system, a enhanced result can be got. The paper affirms the Captive Trajectory System can reach a satisfactory result by coordinative control of two revolve axis without improve the machining accuracy and assembly accuracy.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yan Shi
AU  - Zongzheng Liu
AU  - Xinmin Liu
AU  - Hongwei Han
PY  - 2015/12
DA  - 2015/12
TI  - The amendatory method of three dimensional rotary mechanisms
BT  - Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
PB  - Atlantis Press
SP  - 364
EP  - 367
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmse-15.2015.67
DO  - 10.2991/icmse-15.2015.67
ID  - Shi2015/12
ER  -