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| H－I运载火箭控制系统 | |
| 引用本文： | 张振华.H－I运载火箭控制系统[J].航天控制,1996(1). |
| 作者姓名： | 张振华 |
| 摘 要： | Ｈ－Ｉ运载火箭概况、主要技术性能以及控制系统的配置和功能在文中作了介绍。详细介绍了惯性测量装置、陀螺仪、加速度表、数据接口单元等。最后介绍了系统工作和飞行试验结果。 |
| 关 键 词： | 运载火箭，控制系统，惯性测量装置，飞行试验结果 |
Control System for H-I Launch Vehicle |
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| Zhang Zhenghua.Control System for H-I Launch Vehicle[J].Aerospace Control,1996(1). | |
| Authors: | Zhang Zhenghua |
| Institution: | Zhang Zhenghua |
| Abstract: | The outline, main performance, configuration and function of control sys tem of H-I launeh vehicle, are presented in the paper.The inertial measurement unit, gyro, accelerometer and data interface unit etc are also introduced in detail, Finally, thispaper recommends system operation and flight test result. |
| Keywords: | Launch vehicle Control system Inertial measurement unit Flight test result |
| 本文献已被 CNKI 等数据库收录！ | |