| 基于刚体转动四元数模型的航天器再定向方案 |
| |
| 引用本文： | 刘辉,伍斯宾斯基.基于刚体转动四元数模型的航天器再定向方案[J].航天控制,2000,18(2):22-27. |
| |
| 作者姓名： | 刘辉 伍斯宾斯基 |
| |
| 作者单位： | 乌克兰哈尔科夫国立工业大学 |
| |
| 摘 要： | 介绍了一种新的刚体转动的四元数模型。这些模型可以提高再定向控制的对边界条件的适应能力，在此基础上还介绍了这些模型的一些实际应用。
|
| 关 键 词： | 航天器 定向 刚体 转动 |
| 修稿时间： | 2000-01-12 |
Approach of Orientation of Spacecraft on the Basis of Quaternary Models of Rotation of Rigid Body |
| |
| Liu Hui
,U. B. Usbinski.Approach of Orientation of Spacecraft on the Basis of Quaternary Models of Rotation of Rigid Body[J].Aerospace Control,2000,18(2):22-27. |
| |
| Authors: | Liu Hui U B Usbinski |
| |
| Institution: | Liu Hui
,U. B. Usbinski
(Kharkov State Polyteehnieal University, Department of Automatic Control of Motion) |
| |
| Abstract: | This paper is concerned with the problem of orientation of rigid body. A new kinematics descripiion, which is on the basis of quatemary model of rotation, is decided. Some models of rotation, which can increase the applicability of task of orientation, are designed. Some applications on the basis of these models are presented. |
| |
| Keywords: | Spacecraft Orientation Rigid body Rotation |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
