鸭翼导弹线性二次镇定系统

Engineering Mechanics 2019 Pub Date : 2019-05-13 DOI:10.21495/71-0-73

W. Bużantowicz

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引用次数: 2

摘要

本文研究了鸭控导弹的线性二次镇定系统。本文还提出了一种在反馈回路中选择增益矩阵加权元素的解析方法，从而消除了对Riccati方程的迭代求解。采用模拟试验对提出的解决方案进行了评估。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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A LINEAR-QUADRATIC STABILIZATION SYSTEM FOR A CANARD-CONTROLLED MISSILE

: This paper examines a linear-quadratic stabilization system for a canard-controlled missile. An analytical method for selecting the weighting elements of the gain matrix in the feedback loop is also proposed, eliminating the need for an iterative solution to the Riccati equation. The proposed solution was evaluated using simulation tests.

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来源期刊

Engineering Mechanics 2019

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