摘要
针对空间杀伤器高速交会条件下的末制导问题,首先在建立空间杀伤器动力学模型的基础上,基于相对运动方程设计了采用指数趋近律的变结构制导律,然后进行了平滑处理以抑制系统抖动,最后采用Schmitt触发器对制导指令进行了脉宽调制。仿真结果表明:针对空间目标杀伤变结构制导律具有鲁棒性强、脱靶量小和燃料消耗低的优势,证明了该方法的有效性。
The terminal guidance law for space kill vehicle in high-speed encounter was studied.Firstly,dynamic models of space kill vechicle were established.Then the variable structure guidance law was designed adopting exponential approach law based on the relative motion equation,and chattering was weakened through smoothing.Lastly,pulse width modulation was conducted for guidance command by Schmitt Trigger.The simulation results showed that the guidance law against space target presented in this paper was effective,which had the merits:strong robustness,small miss distance,and low fuel consumption.
作者
臧月进
李仁俊
曾亮
ZANG Yuejin;LI Renjun;ZENG Liang(Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109,China)
出处
《空天防御》
2019年第1期37-41,共5页
Air & Space Defense
基金
上海市自然科学基金(编号16ZR1415900)
关键词
杀伤器
变结构
变轨
末制导律
视线转率
kill vechicle
variable structure
orbital transfer
terminal guidance law
rates of line-of-sight