Component-Based Modeling and Simulation of Compound-Axis Tracking Systems
Yufang Yue, Xiaogang Xie, Jianzhu An, Feizhou Zhang, Jianzhu Zhang
Available Online January 2016.
- https://doi.org/10.2991/icaita-16.2016.82How to use a DOI?
- simulation; compound axis; servo system; driver decoupling
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
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 - https://doi.org/10.2991/icaita-16.2016.82 ID - Yue2016/01 ER -