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Nonlinear Control Design for a Supercavitating Vehicle

机译:超空泡车辆的非线性控制设计

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摘要

Supercavitating vehicles can achieve very high speed but also pose technical challenges in system stability, maneuvering, and control. Compared to a fully-wetted vehicle for which substantial lift is generated due to vortex shedding off the hull, a supercavitating vehicle is enveloped by gas surface (cavity) and thus the lift is provided by control surface deflections of the cavitator and fins, as well as planing force between the vehicle and the cavity. The nonlinearity in modeling of the cavitator, fins, and especially in modeling of the planing force makes the control design more difficult. In this paper, we investigate several nonlinear control design approaches such as sliding-mode control and quasi linear-parameter-varying control for the dive-plane dynamics of a supercavitating vehicle model. The stability and robustness of the final designs are analyzed. Since only a partial set of state variables are measurable, a high-gain observer is also designed to estimate state variables that are not directly available for feedback. Considering the physical limits of deflection angles of control surfaces of the cavitator and fins, we design a saturation compensator and activate it when needed. Then simulation results are presented for the (partial) output feedback controllers, which are combination of state-feedback nonlinear controllers and the high-gain observer.
机译:超空化车辆可以实现非常高的速度,但也给系统稳定性,操纵和控制带来技术挑战。与完全湿润的车辆相比,由于涡流从船体脱落,产生了很大的升力,超空化的车辆被气体表面(空腔)包围,因此升空是由空化器和散热片的控制表面偏转提供的。作为车辆和型腔之间的平面力。空化器,翅片的建模中的非线性,尤其是刨削力的建模中的非线性,使得控制设计更加困难。在本文中,我们研究了针对超空化飞行器模型的潜水面动力学的几种非线性控制设计方法,例如滑模控制和准线性参数变化控制。分析了最终设计的稳定性和鲁棒性。由于只能测量部分状态变量,因此还设计了一个高增益观察器来估计不能直接用于反馈的状态变量。考虑到空化器和鳍片控制面的偏转角的物理限制,我们设计了一个饱和补偿器,并在需要时将其激活。然后给出了(部分)输出反馈控制器的仿真结果,这些输出反馈控制器是状态反馈非线性控制器和高增益观测器的组合。

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