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考虑禁飞区规避的预测校正再入制导方法

赵江 周锐 张超

赵江, 周锐, 张超等 . 考虑禁飞区规避的预测校正再入制导方法[J]. 北京航空航天大学学报, 2015, 41(5): 864-870. doi: 10.13700/j.bh.1001-5965.2014.0488
引用本文: 赵江, 周锐, 张超等 . 考虑禁飞区规避的预测校正再入制导方法[J]. 北京航空航天大学学报, 2015, 41(5): 864-870. doi: 10.13700/j.bh.1001-5965.2014.0488
ZHAO Jiang, ZHOU Rui, ZHANG Chaoet al. Predictor-corrector reentry guidance satisfying no-fly zone constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 864-870. doi: 10.13700/j.bh.1001-5965.2014.0488(in Chinese)
Citation: ZHAO Jiang, ZHOU Rui, ZHANG Chaoet al. Predictor-corrector reentry guidance satisfying no-fly zone constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 864-870. doi: 10.13700/j.bh.1001-5965.2014.0488(in Chinese)

考虑禁飞区规避的预测校正再入制导方法

doi: 10.13700/j.bh.1001-5965.2014.0488
基金项目: 国家自然科学基金(61273349,61175109,61203223,61333004);航空科学基金(2013ZA18001);北航博士研究生创新基金(YWF-14-YJSY-013)
详细信息
    作者简介:

    赵江(1986—),男,陕西西安人,博士研究生,jzhao@buaa.edu.cn

    通讯作者:

    周锐(1968—),男,湖北钟祥人,教授,zhr@buaa.edu.cn,主要研究方向为飞行器自主控制、多飞行器协同控制.

  • 中图分类号: V448.235

Predictor-corrector reentry guidance satisfying no-fly zone constraints

  • 摘要: 针对升力式高超声速飞行器再入滑翔侧向制导问题,提出了一种考虑禁飞区规避的预测校正制导方法.纵向制导采用落点误差预测与指令校正相结合的方式,不断更新倾侧角的幅值,实时修正轨迹纵程.侧向制导设计了一种倾侧角反转逻辑的切换机制,利用航向角误差走廊和航向角导向区域控制飞行器的侧向运动.CAV-H再入滑翔飞行器制导仿真实例表明,该方法不依赖于标准再入轨迹,能够导引飞行器规避禁飞区约束.Monte Carlo仿真验证表明,在随机初始扰动和误差存在的情况下,该制导方法具有良好的鲁棒性.

     

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出版历程
  • 收稿日期:  2014-08-01
  • 修回日期:  2014-09-26
  • 刊出日期:  2015-05-20

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