Component-Based Modeling and Simulation of Compound-Axis Tracking Systems

DOI

10.2991/icaita-16.2016.82How to use a DOI?

Keywords

simulation; compound axis; servo system; driver decoupling

Abstract

Pointing on a certain point of a dynamic target is demanded by beam director system. Compound-axis servo system must be adopted. A component-based compound axis servo system simulation method is proposed, denoted as the CCASS method. Compound-axis tracking system simulation is an effective expansion on EasyLaser, a primary general software platform for laser system simulation. The circumstance nest of Matlab/Simulink makes the CCASS method adaptive to concrete transfer function as well as complex control system. Furthermore, CCAS method aims at searching out a solution for coupling and decoupling simulation of the main-axis and the sub-axis servos, because there are kinematics coupling and driver decoupling problem in a general beam director. Otherwise, a joint simulation with adaptive optical system is derived, which improves tracking precise forwardly. By CCAS method, no matter how the detectors and controlled mirrors are sited in the optical path, kinematical coupling and driver decoupling are resolved automatically. Simulation results indicate that the proposed CCAS method has the capacity of retaining simulative quality and enhancing the simulative facility and adaptability.

Copyright

© 2016, 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  - Yufang Yue
AU  - Xiaogang Xie
AU  - Jianzhu An
AU  - Feizhou Zhang
AU  - Jianzhu Zhang
PY  - 2016/01
DA  - 2016/01
TI  - Component-Based Modeling and Simulation of Compound-Axis Tracking Systems
BT  - Proceedings of the 2016 International Conference on Artificial Intelligence: Technologies and Applications
PB  - Atlantis Press
SP  - 333
EP  - 336
SN  - 1951-6851
UR  - https://doi.org/10.2991/icaita-16.2016.82
DO  - 10.2991/icaita-16.2016.82
ID  - Yue2016/01
ER  -