这份报纸在输入浸透下面为一只僵硬太空船调查全球态度规定控制的问题。基于有限时间的控制和切换的控制方法的技术,一个新奇全球围住的有限时间的态度规定控制器被建议。在建议控制器下面,太空船态度能在一有限时间到达需要的态度,这被显示出。另外,一个建议态度控制器的界限能被适应提供使活动的任何小水平在实际实现跳了。
This paper investigates the problem of global attitude regulation control for a rigid spacecraft under input saturation. Based on the technique of finite-time control and the switching control method, a novel global bounded finite-time attitude regulation controller is proposed. Under the proposed controller, it is shown that the spacecraft attitude can reach the desired attitude in a finite time. In addition, the bound of a proposed attitude controller can be adjusted to any small level to accommodate the actuation bound in practical implementation.