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A nonlinear application of a Lyapunov technique for assuring global performance bounds

机译:Lyapunov技术在确保全局性能范围方面的非线性应用

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In this paper we consider the stability and perfor mance problem of nonlinear systems using a Lyapunov technique. Upper or lower bounds can be provided assuming that a Lyapunov function satisfies a Hamiltonian inequality for all admissible states. Also, suboptimal control laws with guaranteed performance bounds can be derived with this technique. The technique has been applied on rate and attitude control for sounding rockets. As an example a rate control algorithm is elaborated showing the main ideas pre sented in this paper: 1) the Lyapunov function provides a global performance bound; 2) a control law is derived based on the Lyapunov function; and 3) the candidate Lyapunov function is parametrized and improved bounds are obtained using parameter optimization.
机译:在本文中,我们考虑使用Lyapunov技术的非线性系统的稳定性和性能问题。可以假设Lyapunov函数满足所有可允许状态的哈密顿不等式,即可提供上限或下限。同样,可以用这种技术来推导具有保证性能界限的次优控制定律。该技术已应用于探空火箭的速率和姿态控制。举例说明一个速率控制算法,该算法显示了本文提出的主要思想:1)Lyapunov函数提供了一个全局性能边界; 2)基于李雅普诺夫函数推导控制律; 3)对候选Lyapunov函数进行参数化,并使用参数优化获得改进的边界。

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