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- Optimal Sliding Mode Guidance Law Design with Terminal Angle Constraint for Airborne Dispenser 带末端角约束的机载布撒器最优滑模制导律设计
- Slide mode guidance law 滑模制导律
- Guidance Law Design Based on Extended Sliding Mode Control 基于扩展滑动模态控制的末制导律设计
- The Design of Ship-to-Ship Missile Guidance Law Based on Slide Mode Technique 基于滑模技术的舰舰导弹导引律设计
- adaptive sliding mode guidance 自适应滑模制导
- Time mode, Still mode and Auto slide mode. 展示图片模式:时间模式,静态模式,自动展示图片模式。
- Click the icon to enter the Image Slide mode. 单击图标""进入幻灯片浏览模式;
- The chattering of variable structure controller with sliding mode is reduced by using exponential reaching law with saturation function. 采用指数趋近律与饱和函数相结合的方法对滑模控制器的抖振进行了有效抑制。
- Firstly, under the condition that the nonlinear dynamic function of the systems is estimable and bounded, sliding mode control law is presented. 首先，在系统的非线性动态函数满足可估计和有界两个基本假设的条件下，给出了此类系统基于非线性动态函数估计的一般滑模控制律设计。
- A strategy for integral separation PID sliding mode control is proposed. 摘要提出一种积分分离PID滑模控制策略。
- The Application of Fuzzy Sliding Mode Control in Network Congestion Control P. 模糊滑模控制在网络拥塞控制中的应用。
- Simulation results show that the performance of the designed guidance law is superior to that of TPN and APN, and close to that of OPG. 仿真研究表明，该导引律性能优于TPN，APN，接近OPG。
- In this paper, the precise initial guidance law based on velocity gain guidance and the state transition matrix for orbit interception were proposed. 摘要对于轨道拦截问题，给出了一种基于速度增益制导和状态转移矩阵的精确初制导方法。
- The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law. 该初制导方法能补偿制导方法误差和轨道摄动对拦截脱靶量的影响。
- A midcourse guidance law based on zero effort miss forecasting is presented for intercepting a high-speed target in three-dimensional space. 针对三维空间内的高速飞行目标,提出了一种基于预测零控脱靶量的中制导段导引方法。
- Using adaptive sliding mode control principle, hysteretic compensation control law is calculated in order to guarantee the actual hysteresis characteristics to reach the expected linear output. 采用自适应滑模控制原理求取迟滞补偿控制量，以保证实际的迟滞特性能够达到期望的线性输出特性。
- Abstract Optimal guidance law for a torpedo impacting vertically on a maneuvering evader in three dimensions is studied. 摘要 本文研究了三维空间中鱼雷垂直命中机动目标的最优导引律设计问题。
- Applying the optimal guidance law in this paper to a reentry warhead, this optimal control law was proved effective through computer simulation. 将此最优制导算法应用到某型再入弹头，通过计算机仿真验证了算法的正确性。
- A dynamical-integral sliding mode control approach was proposed for the speed controlling of AC servo system. 针对交流伺服系统速度控制问题,提出了一种动态积分滑模控制方法。
- A variable structure midcourse guidance law with terminal angle constraint is proposed, based on the concept of virtual target. 基于虚拟目标的概念,提出了一种带落角约束的变结构中制导律。
