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机动飞行器再入的变结构导引控制
引用本文:詹宏.机动飞行器再入的变结构导引控制[J].航天控制,1992(3).
作者姓名:詹宏
作者单位:北京控制与电子技术研究所
摘    要:本文针对机动飞行器在再入阶段的制导问题提出了一种变结构的闭环导引控制方案.仿真计算结果表明,这种控制方法对于飞行器各种参数的变化具有较好的鲁棒性.

关 键 词:机动航天器  再入飞行器  制导

Re-entry Guidance with Variable structure for Maneuverable Vehicle
Zhan HongBeijing Institute of Control and Electronic Technology.Re-entry Guidance with Variable structure for Maneuverable Vehicle[J].Aerospace Control,1992(3).
Authors:Zhan HongBeijing Institute of Control and Electronic Technology
Institution:Zhan HongBeijing Institute of Control and Electronic Technology
Abstract:The paper presents a closed loop control concept with variable structure for re-entry gnidance of the maneuverable vehicle. Its mathematical simulation results show that the concept provides better robustness for various changes of the vehicle parameters.
Keywords:Maneuverable spacecraft Reentry vehicle Guidance
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