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Study on control strategies for an antenna servo system on a carrier under large disturbance

机译:大扰动下载波天线伺服系统的控制策略研究

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摘要

In this paper, control strategies and vibration isolation methods are investigated in order to enhance the attitude control accuracy of an antenna servo system on a carrier under large disturbance. First, the multi-body dynamical equations of the antenna servo system on a carrier incorporated with six wire-cable vibration isolators are derived. Then, an improved adaptive variable-rated exponential reaching law is proposed, and the non-singular terminal sliding mode control is designed based on the nonlinear multi-body model. Finally, simulations are carried out and results show that excellent control accuracies for both the azimuth and the pitch of the antenna can be achieved by the proposed control method, specifically with a shorten reaching time in the cases of holding a fixed angle and tracking a sinusoidal motion that is better than the existing adaptive variable-rated exponential reaching law. Furthermore, the six wire-cable vibration isolators with hysteretic characteristics of restoring forces are adopted that can effectively isolate the large disturbance transmitted from the carrier to the antenna servo system and are shown to be able to further improve the attitude control accuracy.
机译:在本文中,研究了控制策略和振动隔离方法,以提高在大扰动下载体上天线伺服系统的姿态控制精度。首先,推导出与六个线缆振动隔离器的载体上的天线伺服系统的多体动态方程。然后,提出了一种改进的自适应可变额定指数达到规律,并且基于非线性多体模型设计了非奇异终端滑动模式控制。最后,进行仿真,结果表明,通过所提出的控制方法可以实现各方位角和天线间距的优异控制精度,具体地,在保持固定角度和跟踪正弦的情况下,特别是在缩短达到的时间运动比现有的自适应可变额定指数达成法更好。此外,采用具有滞后特性的六个线缆隔振器,其可以有效地将从载波传递到天线伺服系统的大的扰动,并且被示出能够进一步提高姿态控制精度。

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