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.
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.
出处
《航天控制》
CSCD
北大核心
1992年第3期1-7,共7页
Aerospace Control
关键词
航天器
再入飞行器
制导
Maneuverable spacecraft Reentry vehicle Guidance
