| 无人机着陆控制的特征结构配置方法实现 |
| |
| 引用本文： | 宋辉.无人机着陆控制的特征结构配置方法实现[J].航空计算技术,2009,39(2):21-24. |
| |
| 作者姓名： | 宋辉 |
| |
| 作者单位： | 西北工业大学自动化学院,陕西西安,710072 |
| |
| 摘 要： | 针对无人机纵向着陆系统的控制需求，采用特征结构配置方法的设计方案。阐述了全状态反馈理论基础上的特征结构配置的原理以及根据设计指标确定特征结构配置的方法，并对某型无人机纵向飞控系统动态响应进行分析，给出仿真实例。仿真结果表明，应用特征结构配置方法设计出的控制器，能够使飞机准确地跟踪期望轨迹，满足系统动态性能要求。在工程中具有一定的实用价值
|
| 关 键 词： | 无人机 飞行控制 特征结构配置 仿真 |
Implementation of Eigenstructure Assignment Method in Landing Control for UAV |
| |
| SONG Hui.Implementation of Eigenstructure Assignment Method in Landing Control for UAV[J].Aeronautical Computer Technique,2009,39(2):21-24. |
| |
| Authors: | SONG Hui |
| |
| Institution: | SONG Hui( College of Automatic Control, Northwestern Polytechnical University, Xi＇an 710072, China ) |
| |
| Abstract: | The design for eigenstructure assignment method is proposed in allusion to the control requirement of UAV longitudinal landing system.It analyzes the dynamic response of certain UAV longitudinal flight control system on the basis of full-state feedback theory.This paper theoretically outlines the principle and method of eigenstructure assignment based on design indexes.The simulation is given and the results indicate that flight controller by this method facilitates the plane to track the desired trajectory... |
| |
| Keywords: | UAV flight control eigenstructure assignment simulation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
