| 飞行器数字姿态控制系统频域综合 |
| |
| 引用本文： | 李明华.飞行器数字姿态控制系统频域综合[J].航天控制,1990(1). |
| |
| 作者姓名： | 李明华 |
| |
| 作者单位： | 北京航天自动控制研究所 |
| |
| 摘 要： | 本文提出了频域Z平面直接设计方法的说明。用于设计飞行器数字姿态控制系统数字控制器。首先,讨论了五种典型的数字滤波器,它们具有特定的频域响应。然后用该方法设计一个战术弹道导弹姿态控制系统,获得了递归式——非递归式校正滤波器,它们具有满意的频域响应。
|
| 关 键 词： | 姿态控制系统 数字控制系统 数字滤波器 |
FREQUENCY-DOMAIN DESIGN METHOD FOR FLIGHT VEHICLE DIGITAL ATTITUDE CONTROL SYSTEM |
| |
| Li Minghua Beijing Aerospace Automatic Control Institute.FREQUENCY-DOMAIN DESIGN METHOD FOR FLIGHT VEHICLE DIGITAL ATTITUDE CONTROL SYSTEM[J].Aerospace Control,1990(1). |
| |
| Authors: | Li Minghua Beijing Aerospace Automatic Control Institute |
| |
| Institution: | Li Minghua Beijing Aerospace Automatic Control Institute |
| |
| Abstract: | This paper presents the instruction and illustration of the frequency-domain Zplan direct methodology (FZDD) for designing the digital controller of a flight vehicle digital attitude tontrol system. At first, five basic digital filters with special frequency responses are described. And then ,the FZDD is used to design a tactical ballistic missile attitude control system. The recursive and nonrecursive corrective filters with satisfactory frequency responses are obtained. |
| |
| Keywords: | Attitude control system Digital control system Digital filter |
| 本文献已被 CNKI 等数据库收录！ |
