| 三框架四轴惯性平台系统弹体姿态角解算方法 |
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| 引用本文： | 刘 静,闫 禄,郭宗本,朱志刚.三框架四轴惯性平台系统弹体姿态角解算方法[J].导航与控制,2015,14(2):64-69. |
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| 作者姓名： | 刘 静 闫 禄 郭宗本 朱志刚 |
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| 作者单位： | 北京航天控制仪器研究所,北京,100039 |
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| 摘 要： | 三框架四轴平台虽然满足了导弹武器系统全姿态机动的需求,但由于增加了一个框架角,弹体姿态的解算却比三轴平台复杂得多.根据随动回路的工作特点,推导出了三框架四轴惯性平台系统各种工况下由四个框架角输出解算弹体的三个姿态角的公式.
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| 关 键 词： | 三框架四轴惯性平台 姿态解算 导弹 平台框架 |
Missile Attitude Calculating
of Four-axes Stabled Inertial Platform |
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| LIU Jing,YAN Lu,GUO Zong-ben and ZHU Zhi-gang.Missile Attitude Calculating
of Four-axes Stabled Inertial Platform[J].Navigation and Control,2015,14(2):64-69. |
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| Authors: | LIU Jing YAN Lu GUO Zong-ben and ZHU Zhi-gang |
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| Institution: | Beijing Institute of Aerospace Control Devices;Beijing Institute of Aerospace Control Devices;Beijing Institute of Aerospace Control Devices;Beijing Institute of Aerospace Control Devices |
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| Abstract: | Depending on the 4th frame, the 4-axes stabled inertial platform realizes all attitude maneuverability of the missile, but at the same time the missile attitude calculating becomes more complicated than the 3-axes platform. In this paper, a missile attitude calculating method under all kinds of conditions using the 4 angle sensors of 4-axes stabled inertial platform is presented. |
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| Keywords: | 4-axes stabled inertial platform attitude calculating missle platform frames |
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