| 再入机动飞行器的控制系统设计 |
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| 引用本文： | GUO Zhen-yun,郭振云,雷光新,赵汉元.再入机动飞行器的控制系统设计[J].飞行力学,2005,23(1):61-64. |
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| 作者姓名： | GUO Zhen-yun 郭振云 雷光新 赵汉元 |
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| 作者单位： | 国防科技大学,航天与材料工程学院,湖南,长沙,410073 |
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| 摘 要： | 基于再人机动飞行器机动控制特点，设计了两种反馈结构——过载反馈和姿态角反馈的姿控系统．并从输入反馈信号构成、系统回路设计、反馈系数确定及飞行弹道仿真结果等方面，对两种形式的姿控系统进行了比较。结果表明．过载反馈系统在再人机动飞行器的飞行控制中效果较好。
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| 关 键 词： | 再入机动飞行器 飞行控制 系统设计 过载反馈 姿态反馈 |
| 文章编号： | 1002-0853(2005)01-0061-04 |
| 修稿时间： | 2004年3月10日 |
Control System Design of a Maneuverable Reentry Vehicle |
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| GUO Zhen-yun.Control System Design of a Maneuverable Reentry Vehicle[J].Flight Dynamics,2005,23(1):61-64. |
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| Authors: | GUO Zhen-yun |
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| Abstract: | Based on the maneuverable flight character of the reentry vehicle, two attitude control system with attitude and overload feedback structure are designed, and we have made a comparision between these two systems(including input feedback signals, system loop design, feedback parameters and the simulation of six degrees of freedom). The results shows that the overload feedback structure is better than the attitude feedback structure on the maneuverable flight control. |
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| Keywords: | maneuverable reentry vehicle flight control control system design overload feedback attitude feedback |
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