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满足多约束的主动段能量管理制导方法

徐衡 陈万春

徐衡, 陈万春. 满足多约束的主动段能量管理制导方法[J]. 北京航空航天大学学报, 2012, 38(5): 569-573.
引用本文: 徐衡, 陈万春. 满足多约束的主动段能量管理制导方法[J]. 北京航空航天大学学报, 2012, 38(5): 569-573.
Xu Heng, Chen Wanchun. Energy management ascent guidance algorithm with multiple constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(5): 569-573. (in Chinese)
Citation: Xu Heng, Chen Wanchun. Energy management ascent guidance algorithm with multiple constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(5): 569-573. (in Chinese)

满足多约束的主动段能量管理制导方法

详细信息
  • 中图分类号: V 448.13

Energy management ascent guidance algorithm with multiple constraints

  • 摘要: 高超音速飞行器运载任务需要满足多项约束条件,针对耗尽关机型固体运载火箭需要在主动段进行能量管理.基于控制推力和速度之间夹角来实现主动段能量管理的思路,综合交变姿态控制能量管理(AEM,Alternate Attitude Control Energy Management)和一般能量管理(GEM,General Energy Management),提出了样条能量管理(SEM,Spline Energy Management)制导方法,并针对分离前定轴飞行约束条件进行了修正.以三级运载火箭为例,通过AEM,GEM和SEM对比,验证了样条能量管理制导方法的可行性.

     

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出版历程
  • 收稿日期:  2011-01-26
  • 网络出版日期:  2012-05-30

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