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- Nonlinear robust guidance law 非线性鲁棒制导律
- A robust midcourse guidance law based on the zero effort miss is designed for the middle flying stage of exo-atmospheric intercept with the fuel-exhaustion-shutoff solid engine. 摘要针对大气层外拦截中段采用耗尽关机固体燃料发动机的情况，设计了基于零控脱靶量的鲁棒中制导律。
- The nonlinear robust control method is adopted in advanced static VAR generator (ASVG) control. 将非线性鲁棒控制方法用于先进的静止无功发生器(ASVG)的控制。
- With the aid of the theory of Active Disturbances Rejection Control (ADRC) a nonlinear robust controller designed is presented. 提出了一种运用自抗扰控制理论设计的非线性鲁棒控制器。
- Some background knowledge for nonlinear robust fault-tolerant control, such as nonlinear system theory, robust control and adaptive control, are firstly introduced. 首先介绍了一些与非线性鲁棒容错控制密切相关的研究方向，包括非线性系统理论、鲁棒控制、自适应控制等。
- 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。
- Finally,based on a 2-area 4-machine power system,dynamic simulations are carried out to make a comparison between the effects of AVR+ PSS excitation system and the two nonlinear robust controllers in improving transient stability of the system. 最后采用2区4机系统进行了动态仿真,以比较这2种鲁棒控制器以及自动电压调节器+电力系统稳定器(AVR+PSS)励磁系统在提高电力系统暂态稳定性方面的控制功效。
- 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。
- Based on RBF neural networks and backstepping control techniques, a nonlinear robust controller design method is proposed for missile control systems with input unmodeled dynamics in pitch channel. 在导弹系统俯仰通道中存在输入未建模动态情况下,提出了一种基于RBF神经网络和反演控制技术的非线性鲁棒控制器的设计方法。
- 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。
- 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 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。
- A closed form initial guidance law based on feed forward and feedback neural network control for finite propulsive reentry spacecraft was presented. 提出了一种前馈反馈神经网络闭路初制导律。
- Design of a Nonlinear Robust Self-tuning Controller 一类非线性系统的鲁棒自校控制器设计
- Traditional guidance law of underwater autoguide weapon had lots of defects,which was unsuitable for the tactical requirement of modern torpedoes. 水下声自导武器的传统导引方式存在着种种缺点,已经不适合现代鱼雷的战术要求。
- Nonlinear robust control of maglev train 磁悬浮列车的非线性鲁棒控制
- Proportional navigation(PN)is used as the guidance law for the guided projectile on which SINS/GPS and terminal homing system are adopted. 针对采用SINS/GPS和末端寻的复合制导的制导炮弹,采用比例导引作为中制导和末制导的导引规律。
- Nonlinear Robust Control of Vehicle BTT 飞行器倾斜转弯的非线性鲁棒控制
