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滑翔再入飞行器横侧向耦合姿态控制策略

史丽楠 李惠峰 张冉

史丽楠, 李惠峰, 张冉等 . 滑翔再入飞行器横侧向耦合姿态控制策略[J]. 北京航空航天大学学报, 2016, 42(1): 120-129. doi: 10.13700/j.bh.1001-5965.2015.0037
引用本文: 史丽楠, 李惠峰, 张冉等 . 滑翔再入飞行器横侧向耦合姿态控制策略[J]. 北京航空航天大学学报, 2016, 42(1): 120-129. doi: 10.13700/j.bh.1001-5965.2015.0037
SHI Linan, LI Huifeng, ZHANG Ranet al. Gliding reentry vehicle lateral/directional coupling attitude control strategy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 120-129. doi: 10.13700/j.bh.1001-5965.2015.0037(in Chinese)
Citation: SHI Linan, LI Huifeng, ZHANG Ranet al. Gliding reentry vehicle lateral/directional coupling attitude control strategy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 120-129. doi: 10.13700/j.bh.1001-5965.2015.0037(in Chinese)

滑翔再入飞行器横侧向耦合姿态控制策略

doi: 10.13700/j.bh.1001-5965.2015.0037
基金项目: 国家自然科学基金(61174221,11272062)
详细信息
    作者简介:

    史丽楠女,博士研究生。主要研究方向:高超声速飞行器姿态控制。Tel.:010-82339527E-mail:shi_linan@163.com;李惠峰女,博士,教授,博士生导师。主要研究方向:高超声速飞行器制导与控制。Tel.:010-82319276E-mail:lihuifeng@buaa.edu.cn;张冉男,博士,讲师。主要研究方向:高超声速飞行器制导与控制。Tel.:010-82339527E-mail:zhangran@buaa.edu.cn

    通讯作者:

    李惠峰,Tel.:010-82319276E-mail:lihuifeng@buaa.edu.cn

  • 中图分类号: V448.22

Gliding reentry vehicle lateral/directional coupling attitude control strategy

Funds: National Natural Science Foundation of China (61174221, 11272062)
  • 摘要: 针对气动舵面仅为两片体襟翼的欠驱动构型可重复使用运载器(RLV)再入过程中的强耦合现象,提出一种基于此类布局飞行器耦合特性的横侧向控制策略。在分析惯性耦合、运动耦合和稳定性耦合的产生机理与规避方式的基础上,计算标称轨迹下的急滚稳定边界并将倾侧角指令速率限制在此边界内以稳定惯性耦合;针对现有的荷兰滚模态预测式不适用于此布局飞行器的问题推导出一种新的荷兰滚运动预判方法,并根据预判结果设计控制增益。最终得到低动压下体襟翼-反作用力控制系统(RCS)复合控制策略和高动压下体襟翼单独作用的横侧向耦合控制策略。六自由度(6-DOF)仿真结果表明该控制策略能很好地跟踪制导指令并且能最大限度利用气动舵面以减少RCS燃料的消耗。

     

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出版历程
  • 收稿日期:  2015-01-20
  • 刊出日期:  2016-01-20

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