| 单词 | guidance law | ||||||||||||||
| 释义 | guidance law
更多释义 收起释义 例句释义: 导引规律,制导规律,导引律 1. An UAV maneuver flight trajectory tracking system consists of a guidance law as an outer loop and a flight control as an inner loop. 对无人机机动飞行轨迹跟踪系统的内环姿态控制律和外环轨迹跟踪控制律两部分分别进行了设计。 www.ceps.com.tw 2. The guidance law right to intercept moving targets is of a highly adaptive and a kind precision guided law with practical value. 并且对拦截机动目标有很强的自适应性，是一种具有工程实用价值的高精度末制导律。 www.fabiao.net 3. The guidance law design is simple, without relying on a stored reference trajectory, and could be used for spacecraft's autonomous guidance. 该制导算法设计简单，无须预存参考轨道，能够实现飞行器的自主制导，并且具有燃料消耗次优的特点。 xuebao.jlu.edu.cn 4. Guidance law proposed can be implemented conveniently in engineering as it needs little target information. 该制导律所需测量的目标信息少，易于工程实现。 www.mct.com.cn 5. The simulation shows that the guidance law can complete well the guidance task and ensure the fighter is in a favored attack position. 仿真结果表明：该导引方法在保证所导引飞机处于有利的攻击位置的条件下能够很好地完成飞机的导引。 www.ceps.com.tw 6. When targets fly with non-maneuvering, the optimal guidance law is the proportional guidance law with a changeable factor. 当目标作非机动飞行时，最优制导律是一种变比例系数的比例制导。 hkxb.buaa.edu.cn 7. The digital simulation was compared with the proportional guidance law of terminal angular constraint. 通过数字仿真，并与有末端姿态角约束的修正比例导引律进行对比。 www.71155.com 8. A novel guidance law is devised for developing the guidance technology of optimal glide of a hypersonic reentry vehicle. 针对高超声速再入飞行器最远距离滑翔制导关键技术，设计了一种新型制导律。 lib.cqvip.com 9. A midcourse guidance law for an exo-atmospheric interceptor with constant sustaining thrust shut-off by fuel exhaustion is proposed. 针对采用燃料耗尽方式关机且具有持续定常推力的大气层外拦截弹设计了中段制导律。 www.dictall.com 10. Motion tracking variable structure control theory is applied to design guidance law for passive homing -missiles. 应用运动跟踪变结构控制理论设计被动式寻的导弹的制导律。 dictsearch.appspot.com 1. The simulation results prove that the proposed optimal terminal guidance law can improve the terminal impact angle with precise guidance. 仿真结果表明该最优末制导律在满足制导精度要求下提高了末端入射角。 www.71155.com 2. Finally, taking the predictive fixed time guidance law as an example, analyze the influence of the bias of subsystem to the guidance law. 以固定开机时间预测制导律为例，分析了姿态机动误差、导航误差以及机动执行误差等误差源对制导律的影响。 www.boshuo.net 3. Simulation results show the guidance law proposed can dramatically reduce the landing point error resulting from aerodynamic model errors. 仿真结果表明所设计的制导律可以大幅度减小由于气动模型误差而引起的落点偏差。 www.ceps.com.tw 4. This design method guaranteed better homing performance compared with the proportional guidance law and traditional DGL. 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。 lib.cqvip.com 5. Simulation results show that the proposed guidance law can satisfy the guidance precision requirements of BTT missiles. 仿真表明，所设计的制导律能够满足BTT导弹精确制导的要求。 hkxb.buaa.edu.cn 6. Finally, the virtual displacement guidance law applied in hypersonic craft terminal-guidance was analyzed by simulation. 最后，对虚位移制导律在高超声速飞行器末端段制导中的应用进行了数值仿真分析。 www.boshuo.net 7. Then, with the tracking method, we study the guidance law of the aircraft. Eq. (11) gives the guidance law. 采用追踪法对飞行器的制导规律进行了研究，给出仿真结果。 www.ilib.cn 8. The proposed guidance law is effective in compensating for the adverse influence of autopilot lag on guidance accuracy. 该导引律有效地克服了导弹控制系统的动态延迟对制导精度的影响。 hkxb.buaa.edu.cn 9. Finally, the validity of the gliding guidance law is verified through numerical simulations. 最后，利用设计出的滑翔制导律进行了数学仿真。 lib.cqvip.com 10. The trajectory simulation shows the effectiveness of the designed optimal guidance law. 弹道仿真表明了所设计的最优制导律的有效性。 www.magsci.org 1. In question and answer guidance law teaching materials text basically after the appendix has disposed the certain amount essay question. 问答引导法教材中的课文基本上都在附录后配置了一定数量的问答题。 www.5yhua.org 2. A novel three-dimensional(3D) guidance law is proposed for a reentry vehicle with impact angle constraints. 针对再入飞行器带碰撞角约束的末端导引问题，设计了一种新型三维制导律。 hkxb.buaa.edu.cn 3. A new 3-dimensional (3D) guidance law is proposed to deal with the coupling of bank-to-turn (BTT) missile. 针对倾斜转弯（BTT）导弹制导过程中的双通道耦合问题，设计了一种新型三维（3D）制导律。 hkxb.buaa.edu.cn 4. First, this paper analyzes the missile guidance loop, and establish guidance law simulation model. 本文首先分析了寻的导弹制导回路，建立起制导律仿真模型。 www.fabiao.net 5. An guidance law of agile turn of air to air missile in off-borsight launching is discussed. 讨论了空空导弹在大离轴角发射时的快速转弯控制律。 www.dictall.com 6. While fuzzy guidance law with robust, intelligent, is great concerned. 其中模糊制导律鲁棒性强，智能性高，受到很大关注。 www.fabiao.net 7. Based on Fuzzy Neural Network(FNN), an intelligent adaptive sliding-mode guidance law is presented. 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。 www.dictall.com 8. Based on the pursuit guidance law and the proportional guidance law, a new guidance law is proposed for space intercept. 基于追踪导引律和比例导引律，提出了一种新的空间拦截末制导律。 www.ceps.com.tw 9. New guidance law based on latest control theory has become a hot spot in precision guidance technology. 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。 www.boshuo.net 10. Therefore it can be used in design of guidance law for torpedo and anti-torpedo torpedo. 该结果可广泛应用于鱼雷及反鱼雷的导引律设计。 www.juyy.net 1. Traditional homing guidance law can not meet the increasingly strict interception requirements, especially for target with great maneuver. 传统末制导律不能满足日趋严格的拦截要求，尤其是目标大机动规避。 www.fabiao.net 2. The normal orbit in the homing phase is designed based on a C-W guidance law. 采用C-W制导算法，对寻的段飞行任务的标称轨道进行了设计。 www.ceps.com.tw 3. Comparing Study of Proportional Navigation Guidance Law of Attitude and Acceleration Autopilots 姿态及过载自动驾驶仪比例导引对比研究 service.ilib.cn 4. Study of the closed-loop guidance law for boost phase with reentry constraints of maneuvering reentry vehicles 机动再入飞行器主动段再入点约束闭路制导研究 www.ilib.cn 5. study of target acquisition probability for laser - guided bombs with proportional navigation guidance law 激光比例制导航弹对目标的捕获概率分析 www.ichacha.net 6. Research on Maneuvering Penetration Guidance Law of Ballistic Missile in Middle-course Flight by Simulation Method 弹道导弹中段机动突防制导问题的仿真研究 service.ilib.cn 7. Design and Simulation of a Fuzzy Terminal Guidance Law with Robustness to Measurement Noise Disturbances 一种对噪声干扰鲁棒的模糊末制导律设计与仿真 www.ilib.cn 8. The Optimum Intermediate Guidance Law of Missile Considering the Characteristic of Solid Ducted Rocket 考虑冲压发动机特性的导弹最优中制导律研究 service.ilib.cn 9. Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile 一种次优空射巡航导弹中制导律的推导与仿真 www.ilib.cn 10. An Optimal Guidance Law of Maneuvering Reentry Vehicles with Terminal Angular Constraint 具有终端角度约束的机动再入飞行器的最优制导律 service.ilib.cn 1. Initial Guidance Law of Closed-form Neural Network for Maneuverable Reentry Vehicle 机动再入飞行器神经网络闭路初制导研究 scholar.ilib.cn 2. A New Variable Structure Guidance Law of Three Dimensional with Multiple Constraints 一种多约束条件下的三维变结构制导律 www.ilib.cn 3. Design and Simulation for Terminal Guidance Law of Long Range Antiaircraft Missile 中远程防空导弹的末制导律设计与仿真 www.ilib.cn 4. A Midcourse Guidance Law for an Exo-Atmospheric Interceptor with Fuel Exhaustion Shutoff Motor 大气层外拦截弹中段耗尽关机制导律 www.ilib.cn 5. An Engineering Implementation Method of an Optimal Midcourse Guidance Law Using Neural Network 一种神经网络最优中制导规律的工程实现方法 service.ilib.cn 6. Design and Identification on Parameters of Proportional Navigation Guidance Law with Gravity Over Compensation 带过重力补偿的比例导引制导律参数设计与辨识 www.ichacha.net 7. Study on a Variable Structure Guidance Law Against the Escape Maneuvering Target at Endgame 目标末端逃逸的变结构制导律研究 service.ilib.cn 8. Research on Optimal and Perpendicular Impact Guidance Law for Underwater Vehicles with Infinitely Variable Speeds 无级变速鱼雷的最优垂直命中导引律研究 www.ilib.cn 9. Research on Burnout Reference Guidance Law for an Exo-atmospheric Interceptor 大气层外拦截器关机基准制导法研究 www.ilib.cn 10. Trajectory Simulation of Proportional Navigation Guidance Law for Leading Impact Point of Portable Ground-to-Air Missile 便携式地空导弹超前修正导引弹道模型的仿真研究 ilib.cn 1. Robust adaptive variable structure guidance law considering autopilot dynamics 考虑自动驾驶仪动态鲁棒自适应变结构制导律 www.ilib.cn 2. Guidance Law of Reentry Vehicle with Terminal Angular Constraint 再入飞行器的终端角度约束制导律设计 www.ilib.cn 3. Design of Guidance Law of Variable Structure for the Reentry Warhead 再入弹头变结构制导律设计 service.ilib.cn 4. A Study on Pursuit Guidance Law of Trajectory Correction Projectiles 弹道修正弹追踪制导律研究 service.ilib.cn 5. Trajectory tracking guidance law and trajectory simulation of antiballistic missile 防空导弹反弹道导弹跟踪制导规律研究和弹道仿真 www.ilib.cn 6. Research on fuzzy variable structure guidance law for passive homing missiles against maneuvering targets 攻击机动目标的被动寻的模糊变结构制导律研究 ilib.cn 7. Modeling of Three-Dimensional Guidance Problems and Guidance Law Design against Maneuvering Targets 机动目标三维空间导引运动建模及导引律研究 service.ilib.cn 8. Modeling and Analysis of the Guidance Loop for the Missile Velocity Pursuit Guidance Law 速度追踪制导律导引回路建模及解析分析 ilib.cn 9. Research on Guidance Law of Air-to-air Missile for High Off-boresight Launch Condition 大离轴角发射空空导弹制导律研究 service.ilib.cn 10. Nonlinear Variable Structure Guidance Law for Realizing Large-space Variable Trajectory 反舰导弹的非线性变结构制导律研究 www.ilib.cn 1. Longitudinal Flight Control and Guidance Law Design for Trans-aerosphere Vehicle During Climbing Phase 跨大气层飞行器爬升段纵向飞行控制律和制导律设计 service.ilib.cn 2. Variable-structure Guidance Law with Terminal Angular Constraint of Video-guided Penetrating Bomb 电视制导侵彻炸弹落角约束变结构制导律 www.ilib.cn 3. Simulation Research on Optimal Sliding-Mode Guidance Law for an Anti-Ship Missile 反舰导弹最优滑模制导律仿真研究 www.ilib.cn 4. The Study of an Optimal Sliding-mode Guidance Law of Fighter Plane 一种载机最优滑模导引律研究 service.ilib.cn 5. The Optimum Intermediate Guidance Law of Long Distance Air-to-Air Missile 远距空空导弹最优中制导律研究 scholar.ilib.cn 6. Research of Combined Terminal Guidance Law and Its Simulations 组合末制导律及其仿真研究 www.ilib.cn 7. An optimal sliding-mode guidance law for modern fighters and its simulation 一种用于现代战斗机的最优滑模导引律及其仿真研究 www.ilib.cn 8. 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 www.ilib.cn 9. Design and Simulation of an Advanced Proportional Guidance Law 一种改进的比例导引规律的设计与仿真 scholar.ilib.cn 10. Research on Three-Dimensional Optimum Guidance Law for Air-to-Air Missile Attacking Maneuvering Target 空空导弹攻击机动目标的三维最优制导律研究 www.ilib.cn 1. Yaw Plane Guidance Law Considering Steady Error Of Control System of a Missile 考虑控制系统稳态误差的导弹航向平面导引律 www.ilib.cn 2. Optimal Trajectories Design and Closed-loop Guidance Law Study for Aero-assisted Space Rendezvous 气动辅助空间交会最优轨道设计与闭环导引律 www.ilib.cn 3. The Design of Guidance Law of Aerodynamic Missile Based on Intelligent Sliding-mode Variable Structure 飞航导弹智能自适应滑模制导律设计 www.ilib.cn 4. Synthesis of fuzzy logic guidance law for homing missiles using evolutionary strategies 基于进化策略的导弹模糊制导律设计 www.ilib.cn 5. An adaptive variable structure guidance law considering missile's dynamics of autopilot 一种考虑自动驾驶仪动态特性的自适应变结构制导律 ilib.cn 6. Guidance Law Design with Terminal Attitude Constraint for Airborne Dispenser 有末端姿态角约束的机载布撒器导引律设计 www.ilib.cn 7. Study of the present status and prospect of the guidance law 制导规律研究现状及展望 service.ilib.cn 8. Design of Terminal Guidance Law for Mass Moment Interceptor with Three-axial Stabilization 三轴稳定质量矩拦截器的末制导律设计 www.ilib.cn 9. A Parameter-Variable Integrated Guidance Law Against Big Maneuvering Target 一种攻击大机动目标的变参数组合导引律 service.ilib.cn 10. Variable Structure Midcourse Guidance Law with Angle Constraint for Anti-Ship Missile 带落角约束的反舰导弹变结构中制导律研究 www.ilib.cn 1. Research on nonlinear terminal guidance law under high alignment angle condition 大配平角起始条件下的非线性末制导律研究 www.ilib.cn 2. Midcourse Guidance Law for an Exoatmospheric Interceptor 大气层外拦截弹中段制导方法研究 www.ilib.cn 3. Research on the Optimal Guidance Law for Realizing Large-airspace Varying Trajectory 实现大空域变轨的最优制导律研究 ilib.cn 4. The Research of Capturing-after-launch Longitudinal Optimal Middle Guidance Law 射后截获纵向最优中制导律研究 service.ilib.cn 5. Study on the ENDGAME Sliding-Mode Guidance Law of Air-to-Air Missile 空空导弹末端控制滑模导引律研究 service.ilib.cn 6. Design of Variable Structure Adaptive Guidance Law for Space Interception 一种变结构自适应空间拦截导引规律设计 www.ilib.cn 7. A Sliding-Mode Guidance Law for Homing-Missiles Breaking Through Defense with Maneuver 导弹机动突防滑模制导律 service.ilib.cn 8. Guidance motion model and guidance law design of the angle-of-attack missile 大攻角导弹的导引运动建模与导引律设计 www.ilib.cn 9. Design of the robust guidance law with terminal angle constraint 具有末端角约束的鲁棒制导律设计 www.ilib.cn 10. Space Shuttle Guidance Law for Terminal Energy Management Flight Phase 航天飞机末端能量管理制导律 www.ilib.cn 1. Design and Simulation of an Intelligent Terminal Guidance Law Based on Direct Lateral Jet Control 基于直接侧向力控制的智能末导引律的设计与仿真 service.ilib.cn 2. Impact Angle and Final Position Constrained Optimal Guidance Law 限制导弹落角和落点的最优制导律 www.ilib.cn 3. Study on Fuzzy Adaptive Sliding-Mode Variable Structure Guidance Law 模糊自适应滑模变结构制导律研究 www.ilib.cn 4. An Integrated Guidance Law for Target Escapes with High Acceleration 一种攻击大机动目标的组合导引律 www.ilib.cn 5. Optimization Design of Fuzzy Logic Control Guidance Law Based on Genetic Algorithm for Pursuit and Interception of Flight Vehicle 基于遗传算法的飞行器追踪拦截模糊导引律优化设计 www.ilib.cn 6. New Three-Dimensional Nonlinear Homing Guidance Law for BTT Missile BTT导弹的新型三维非线性寻的制导律 service.ilib.cn 7. Research on Intelligent Optimal Sliding-Mode Guidance Law 智能化最优滑模制导律研究 service.ilib.cn 8. Study on Optimal Terminal Guidance Law for Maneuvering Targets 攻击机动目标的最优导引规律 www.ilib.cn 9. Design of Guided Air Ammunition's Fuzzy Variable Structure Guidance Law 制导航空弹药模糊变结构制导律的设计 service.ilib.cn 10. The Design of Optimal Fuzzy Guidance Law with Terminal Constraints 具有终端约束的模糊导引律设计 www.ilib.cn 1. The Design of Airborne Dispenser's Variable Structure Guidance Law 机载布撒器变结构制导律的设计 www.ilib.cn 2. Approximate optimal guidance law for aeroassisted plane change problem 气动辅助异面变轨问题中近最优导引律解 service.ilib.cn 3. Study of Optimal IR Passive Guidance Law Based on Extended Kalman Filter 扩展卡尔曼滤波的最优红外被动制导律 service.ilib.cn 4. The Design of Slide Predictive Guidance Law for Guided Air Ammunition 航空弹药滑动预测制导律的设计 www.ilib.cn 5. Modeling and Analysis of Guidance Loop with Body Pursuit Guidance Law 弹体追踪制导律制导回路建模及解析分析 www.ilib.cn 6. Terminal Guidance Law Design in Space Interception 空间拦截的末制导律设计 www.ilib.cn 7. Design of Closed Loop Optimal Guidance Law Using Neural Networks 神经网络最优闭环制导律设计 service.ilib.cn 8. A Hybrid Guidance Law of Intercept and Non-interference Based on Fuzzy Logic 基于模糊逻辑的前置点导引和无干扰导引的混合导引律 www.ilib.cn 9. Design of Guidance Law for Passive Homing Penetrating Bomb 被动寻的式侵彻炸弹的制导律设计 www.ilib.cn 10. A guidance law for air defence missile trajectory tracking 防空导弹弹道跟踪制导规律研究 service.ilib.cn 1. A Precise Initial Guidance Law for Orbit Interception 轨道拦截问题的一种精确初制导方法研究 www.ilib.cn 2. A Terminal Guidance Law Design for Side Jet Control Missile Based on Adaptive Fuzzy Variable Structure Control 直接侧向力控制导弹的自适应模糊变结构末制导律设计 www.ilib.cn 3. An Optimal High-altitude Guidance Law for Reentry Vehicle 再入飞行器高空最优制导律 service.ilib.cn 4. Design of guidance law and controller of missile with terminal angular constraint based on optimal control 基于最优控制的落角约束攻击设计 ilib.com.cn 5. Mid-Course Guidance Law for Long Range Multi-Purpose Missiles 远程多用途导弹中段制导律 service.ilib.cn 6. A Comparing Study Both Body and Velocity Pursuit Guidance Law 两种追踪制导律对比研究 www.ilib.cn 7. Aim Point Guidance Law Design in Space Interception 空间拦截的目标攻击点制导规律研究 www.ilib.cn 8. Design of variable structure terminal guidance law in posture restraint trajectory based on GA 基于GA的带终端约束的变结构末制导律设计 www.ilib.cn 9. A self-adaptive region fuzzy logic guidance law based on Genetic Algorithm and Simulated Annealing 基于遗传退火算法的变论域三维模糊导引律 168.160.184.82:8080 10. The Use of Steepest Ascent Method in Optimal Guidance Law Simulation of Missile 梯度法在导弹最优制导律仿真中的应用 www.ilib.cn 1. Neuro-Optimal Guidance Law for Lunar Soft Landing 月球软着陆的神经元最优制导控制方法 ilib.cn 2. An Integrated Guidance Law Using Fuzzy Logic 基于模糊逻辑的组合导引律 ilib.com.cn 3. Study on New Variable Structure Guidance Law 一种新的变结构制导律研究 www.ilib.cn 4. A Variable Structure Guidance Law Based on Relative Velocity Deflection Angle 基于相对速度偏角的变结构导引律 ilib.cn 5. Missile Trajectory Simulation and Analysis Based on Optimal Guidance Law 导弹最优制导律弹道仿真分析 www.ilib.cn 6. Study on Random Optimal Guidance Law for Air-to-air Missile 空空导弹随机最优导引规律的研究 www.ilib.cn 7. Simulation design of nonlinear pursuit-guidance law based on sliding-mode control 基于滑模控制的非线性追踪导引律仿真设计 ilib.cn 8. An Investigation of Three Dimension Terminal Guidance Law Based on TLC Method for Air-to-air Missile 基于TLC方法的空-空导弹三维末制导律研究 www.ilib.cn 9. A Method of Computing Basic Firing Data of Ballistic Missiles Based on Disturbance Guidance Law 基于摄动制导的弹道导弹发射诸元的仿真算法 www.ilib.cn 10. Trajectory Simulations on Active-Radar-Guided AAM Based on Optimal Guidance Law 基于最优末制导律的主动雷达空空导弹的弹道研究 service.ilib.cn 1. Study on Optimal Terminal Guidance Law for AAM 主动雷达型空空导弹最优末制导律工程研究 ilib.cn 2. Terminal Guidance Law Based on Receding Horizon Control for Homing Missile 基于滚动时域控制的寻的导弹末制导律研究 scholar.ilib.cn 3. Research on the optimal guidance law for antiship missile based on the virtual targets 基于虚拟目标的反舰导弹的最优制导律研究 ilib.cn 4. Study on guidance law for homing missiles 寻的导弹导引规律研究 service.ilib.cn 5. Research on Variable Structure Guidance Law Based on Trending-law for BTT Missile 倾斜转弯导弹的变结构制导律研究 www.ilib.cn 6. Optimal Terminal Missile Guidance Law Based on Fuzzy Neural Networks 基于模糊神经网络的导弹最优寻的末制导律 service.ilib.cn 7. Variable Structure Terminal Guidance Law Based on Zero Miss-distance 基于零脱靶量设计的变结构末制导律 service.ilib.cn 8. Yaw Plane Guidance Law Design Based on Variable Structure Control Theory 基于变结构控制理论的航向平面导引规律设计 www.ilib.cn 9. Guidance Law Based on Fuzzy Variable Structure Control 基于模糊变结构控制的制导律设计 service.ilib.cn 10. 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 www.ilib.cn 1. Research of Precision Guidance Law Based on Q-Learning for Air-to-Air Missile 基于增强学习的空空导弹智能精确制导律研究 www.ilib.cn 2. 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 service.ilib.cn 3. An Optimum Guidance Law Based on Genetic Algorithm 基于遗传算法的最优导引律 www.ilib.cn 4. A New Hybrid Guidance Law Based on Fuzzy Logic 基于模糊逻辑的现在方位导引和无干扰导引的混合导引律 www.ilib.cn |
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