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The approach of partial stabilisation in design of discrete-time robust guidance laws against manoeuvering targets

机译:用于操纵目标的离散时间强大指导法设计的偏稳定方法

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摘要

In this paper, a robust three-dimensional guidance law against manoeuvering targets is designed using the approach of discrete-time partial stabilisation. In the proposed method, the equations of the guidance problem are divided into two subsystems where the asymptotic stability is desired only for the first one. The control input of the second subsystem is designed such that the collision to be ensured in a short time. Despite recent advances in technology and implementation of digital controllers, the design of guidance laws with the approach of discrete-time partial stabilisation has not been done, till now. One of the advantages of this paper is to design a discrete-time guidance law even with the difficulties of the discrete-time Lyapunov theorem. Moreover, the Lyapunov function is chosen based on the physics of the guidance problem (making the rate of line of sight (LOS) rotation close to zero), and it is shown that it is not possible to asymptotically stabilise the system in the case of manoeuvering targets. Nevertheless, to guarantee the collision with the target, it is enough to limit the rotation rate of LOS to a small value. Finally, simulation results are given to show the appropriate performance of the proposed guidance law.
机译:本文使用离散时间部分稳定的方法设计了一种强大的三维指导法。在所提出的方法中,引导问题的方程被分成两个子系统,其中仅对第一个来进行渐近稳定性。第二子系统的控制输入被设计成使得在短时间内确保碰撞。尽管最近的技术和实施数字控制器的进展,但尚未完成具有离散时部分稳定方法的指导法的设计,直到现在。本文的一个优点是设计一个离散时间的指导法,即使是离散时间Lyapunov定理的困难。此外,基于引导问题的物理(使视线(LOS)旋转速度接近零)来选择Lyapunov功能,并且示出了在壳体中不可能渐近稳定该系统修理目标。然而,为了保证与目标的碰撞,它足以将LOS的旋转速率限制为小值。最后,给出了仿真结果表明所提出的指导法的适当表现。

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