摘要
1.前言 激光跟踪系统是航空航天工程中的重要设备之一。要想建造高精度激光跟踪系统,除了提高有关部件的精度之外,系统的综合设计是一个关键步骤。对于这类系统的综合设计,目前都采用全连续或全离散控制方案,而且不考虑对象未建模动态和子系统间的耦合问题。
The laser tracking system is an important device in aeronautical and astronautical engineering, for raising its tracking accuracy the synthetic design of the system is a key procedure. For the synthesis in general the continuous or discrete schemes are adopted to date, and it is difficult to eliminate the effect of unmodeled dynamics in plant and coupling action between subsystems. In this paper a new hybrid adaptive controller is proposed for the laser tracking system with high accuracy, and the controller adapts to the plant with unmodeled dynamics. When the laser tracking system is designed, the coupling action between subsystems should be firstly transfered into unmodeled dynamics in plant, then the hybrid adaptive system should be synthesized according to the procedure proposed in the paper. Both theoretical proof and simulation results demonstrate that the controller can guarantee the robust stability of the closed loop system. Since the hybrid adaptive controller possesses advantages of both continuous and discrete systems, and the tracking error in the system tends to zero, it may be extensively used in aeronautical and astronautical engineering.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1991年第7期A423-A427,共5页
Acta Aeronautica et Astronautica Sinica
关键词
激光跟踪系统
自适应控制
航空
laser tracking system, hybrid adaptive control, unmodeled dynamics, robust stability.