本文研究了一种基于相对速度偏角的导引律。
This paper studies a new guidance law based on the relative velocity deflection Angle.
对两方面的要求需要通过选择合适的导引律来实现。
These demands on the two aspects can only be carried out by selecting suitable guidance law.
基于变结构控制理论，提出了一种垂直命中目标的导引律。
Based on the variable structure control theory, a guidance law that can perpendicularly impact on the target was proposed in this paper.
对要求垂直入射的情况，设计了满足入射角度要求的导引律。
In some cases, there is a requirement of angular at intercept point, a guidance law I...
战机追踪导引性能的关键是其火控系统应具有高性能的导引律。
The key for fighter aircraft to implement target pursuit and interception in an air dogfight is to design high performance guidance law for its fire control system.
在空地导弹的导引律中，比例导引法与直接导引法各有优缺点。
Among the guidance principles of the air-to-ground missile, the proportional guidance method and the direct guidance method have their respective advantages and disadvantages.
基于最新控制理论的新型导引律成为各国精确制导技术的研究热点。
New guidance law based on latest control theory has become a hot spot in precision guidance technology.
基于模糊逻辑理论，本文提出了一种水下航行器模糊前置点线导导引律。
Based on fuzzy logic, a fuzzy intercept wire-guided guidance law of the underwater vehicle is proposed in this paper.
并与一般模糊导引律以及工程中广泛应用的比例导引律进行了性能对比。
The comparison of the performance for the designed guidance law with that of pure fuzzy logic guidance law and proportional guidance law widely used in practical engineering was conducted.
传统的模拟信号导引律已不能满足将数据链的数字接收信号直接应用的要求。
Besides, the analog guidance law can not also apply digital signals come from the data link directly.
所提出的设计方法较比例导引律和传统微分对策导引律具有更好的寻的性能。
This design method guaranteed better homing performance compared with the proportional guidance law and traditional DGL.
依据所建立的系统模型和扩展比例导引算法，利用最优控制理论求出了最优导引律。
Based on the models and the expanded proportion guidance algorithm and by using theory of optimal control, the optimum guidance algorithm is found out.
给出了两种控制方法的导引律，计算了典型弹道的攻角、俯仰角和交班点速度等参数。
The Angle of attack, pitch Angle and velocity at shifted point for typical trajectory were calculated.
其次，在导引段，以脉冲控制策略为前提，分别设计了指数滑移导引律和能量最优转移轨道。
Secondly, the exponential slippage guidance method and optimal energy transfer orbit are designed respectively in the homing phase.
该导引律能同时满足脱靶量要求和末端落角要求，保证了大空域变轨弹道的各段弹道平滑衔接。
This guidance law can satisfy the requirements of miss distance and terminal Angle, thus it guarantees that all phases of the large-space variable trajectory smoothly link.
仿真结果表明：应用此导引律，导引时间短，轨迹较为平直，适用于对现代战斗机的导引控制。
Simulation shows that by the use of this guidance law, the guidance time is shorter and the trajectory is more straight, so it can be applied to the guidance control of modern fighters.
在自适应滑模导引律的基础上，提出了一种基于模糊神经网络(FNN)的自适应滑模导引律。
Based on Fuzzy Neural Network (FNN), an intelligent adaptive sliding-mode guidance law is presented.
针对导弹拦截问题，在非线性系统滑模变结构控制理论的基础上，提计出一种新型滑模变结构导引律；
The missile guidance law utilizing nonlinear variable structure control is proposed. The acceleration command input is determined considering the target acceleration as an uncertainty.
最后，针对自适应模糊导引律参数设计的困难，设计了两种基于RBF神经网络的自适应模糊导引律。
Finally, to the difficulty of the design parameters in adaptive fuzzy guidance law, two adaptive fuzzy guidance laws based on RBF are designed.
根据导弹与目标之间的相对运动方程，应用李雅普·诺夫稳定性理论设计一种新的导弹航向平面导引律。
According to the dynamic equation of relative motion between the missile and the target, Lyapunov stability theory is used to design a new yaw plane guidance law for missiles.
在不同飞行条件下的全弹道仿真结果表明，该导引律均能同时满足布撒器在抛撒点精度和期望姿态角要求。
Finally, full envelope simulation results from different flight conditions show that the guidance law can meet the requirement of both precision and angular constraint of airborne dispenser.
研究表明，由于变结构控制的应用，使得制导律具有很强的鲁棒性，比传统的比例导引律有更多的优越性。
Research shows because of the application of variable structure control, the guidance laws have strong robustness and more advantages over the conventional proportional navigation...
文中在对弹道追踪导引律原理进行简单介绍的基础上，在六自由度弹道模型上进行了蒙特卡洛仿真打靶试验。
Based on the brief introduction of the theory of trajectory tracking guidance law, Monte Carlo simulation fire tests were done with the 6 degree-of-freedom trajectory simulation model.
首先在相对运动学的基础上建立了归一化的导弹—目标的运动学模型，然后利用变结构控制理论设计了导引律。
The unitary missile target kinematics model is established based on the relative kinematics firstly. Then the guidance law is designed using variable structure system theory.
文中基于广泛应用的比例导引律，对目标机动与导引指令信号进行分析，提出了一种直接力引入时机的设计方法。
Based on proportional navigation which is popularly used, target maneuver and guidance command is analyzed, and one design method of beginning time of reaction-jet is proposed.
该导引律在不需要解算目标速度的前提下，通过在线自组织调整航行器的提前角，从而使水下航行器的前置点与目标交会。
This guidance law, without the need of the target velocity, can make the underwater vehicle meet the target in the intercept point by self-organizing adjusting its lead Angle on line.
指数滑移导引律的基本思想是在逼近过程中，保证追踪星的当前位置和终端位置之间的矢量方向不变，而逼近速度逐渐减小；
The spirit of the exponential slippage guidance method is keeping the direction from temporary position to the aiming point while decreasing the approach speed.
最后，采用新型最优制导律和传统比例导引律分别进行了拦截过程的计算机数值仿真，仿真结果表明了这种新型最优制导律的有效性。
Finally, the computer numerical simulation of interceptions adopting optimal guidance law and proportional navigation is processed respectively. The result of simulation shows the perfect...
为了实现反舰导弹的大空域变轨，提出了一种三维虚拟目标比例导引律。该导引律利用简单的控制指令就能控制导弹完成复杂的大空域变轨。
In order to realize large airspace transfer orbital trajectory of an anti-ship missile, a 3-dimensional virtual target's proportional navigation guidance (PNG) law is proposed.
为了实现反舰导弹的大空域变轨，提出了一种三维虚拟目标比例导引律。该导引律利用简单的控制指令就能控制导弹完成复杂的大空域变轨。
In order to realize large airspace transfer orbital trajectory of an anti-ship missile, a 3-dimensional virtual target's proportional navigation guidance (PNG) law is proposed.
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