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Description: 飞机泊位管理系统中单片机代码，实现了飞机上位的自动引导，和预分配能力-aircraft parking management system microcontroller code, the flight upper automatic guidance, and pre-distribution capacity
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Size: 65339 |
Author: 吴飞 |
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Description: 飞机泊位管理系统中单片机代码，实现了飞机上位的自动引导，和预分配能力-aircraft parking management system microcontroller code, the flight upper automatic guidance, and pre-distribution capacity
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Size: 65536 |
Author: 吴飞 |
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Description: 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的
机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的
变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的
制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。
-Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to two two-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal.
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Size: 295936 |
Author: 李恒 |
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Description: 嫦娥一号卫星是中国首颗月球卫星。卫星制导、 导航与控制 (GNC)任务复杂多变 ,对系统实时性、 可靠性和精度要求较高。文章介绍嫦娥一号卫星GNC系统组成、 控制方法、 系统特点和典型飞行结果。-Chang' e One satellite is China' s first lunar satellite. Satellite guidance, navigation and control (GNC) the task is complex and changeable, the system real-time performance, reliability and high precision. In this paper, Chang' e I satellite GNC system, control method, system characteristics and the results of a typical flight.
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Size: 556032 |
Author: 还都 |
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Description: 导弹飞行过程中采用比例导引法，本程序对飞行轨迹就行模拟计算。-Missile flight in the proportional guidance law, the procedures of the flight path on-line simulation.
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Size: 1024 |
Author: caoyj |
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Description: 采用平行接近法对导弹飞行制导过程进行弹道模拟-Parallel close to the method of ballistic missile flight guidance process simulation
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Size: 1024 |
Author: caoyj |
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Description: XML飞行制导控制仿真软件的设计Flight Guidance Control XML design simulation software-Flight Guidance Control XML design simulation software
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Size: 708608 |
Author: dede |
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Description: 导弹内部控制系统的设计。包括导弹制导，导弹飞行，导弹控制，通信传输等等部分。-Missile internal control system design. Including missile guidance, missile flight, missile control, communications, transport and so on parts.
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Size: 6786048 |
Author: 刘睿智 |
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Description: UAV Fault-Diagnosis Systems from Fault Detection to Fault Tolerance-UAV Fault-Diagnosis Systems from Fault Detection to Fault Tolerance
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Size: 5906432 |
Author: piethein |
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Description: 前置量法弹道仿真。前置量法也称角度法或矫直法，采用这种导引方法导引导弹时，在整个飞行过程中，导弹-制导站的连线始终提前于目标-制导站连线，而两条连线之间的夹角 则按某种规律变化。通过建模仿真，使大家更形象生动的理解前置量法。-Front method of trajectory simulation. Front Method, also known as the angle law or straightening method, using this guide guided missile throughout the flight, the missile- guidance station connection is always in advance of target- guidance station connection, while two The connection between the angle between the press some law changes. Through modeling and simulation, more vivid understanding of pre-Method.
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Size: 1024 |
Author: 黄佳琦 |
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Description: paper Vision Based Guidance and Flight Control in Problems of Aerial Tracking
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Size: 3433472 |
Author: top |
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Description: The objective of this chapter is to design a robust controller to achieve outstanding
formation flight of unmanned aerial vehicles and to accurately track the desired path while
facing unknown disturbances. In other words, the goal is to design the autopilot laws to
enforce the desired formation by following the guidance commands. Given a non-linear
mathematical model of a quadrotor (X-shaped rotorcraft), a smooth controller composed of
three time-scaled nested controllers is developed using sliding mode control driven by
sliding mode disturbance observer techniques based on inversion of rotorcraft dynamics
and quaternions mathematical representation.
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Size: 559104 |
Author: nader |
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Description: 利用C语言实现导弹三自由度弹道，制导采用比例导引法，适合导弹飞行力学初学者学习-Using C language to realize three degrees of freedom ballistic missile, guidance using the proportional guidance method, suitable for beginners learning missile flight mechanics
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Size: 1024 |
Author: 杨哲 |
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Description: 空中对准的经典论文，选自《Journal of Guidance，Control and Dynamics》-Aerial alignment classic papers, selected from " Journal of Guidance, Control and Dynamics"
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Size: 1229824 |
Author: wangdingjie |
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Description: 简单的导弹制导模块，根据飞行过程中的误差实时地调整导弹的飞行攻角-Simple missile guidance module, according to the flight of the missile attack angle error adjustment flight in real time
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Size: 50176 |
Author: |
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Description: 简单的导弹制导模块，根据飞行过程中的误差实时地调整导弹的舵机-Simple missile guidance module, according to the flight of the missile servo error adjustment in real time
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Size: 16384 |
Author: |
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Description: 深度学习算法实现（系统能够在较短时间内精确识别障碍物体，时间快为指标）
感知（环境感知）—认知（视觉追踪）—决策（指点飞行）-Deep learning algorithm (the system in a relatively short period of time to accurately identify obstacles that quick time as an indicator)
Perception (context-aware)- cognitive (visual tracking)- Decision (flight guidance)
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Size: 3142656 |
Author: 黄艳虎 |
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Description: 动态规划多弹飞行路经规划与协同制导方法程序-Dynamic Programming Shells flight path planning methods and cooperative guidance program
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Size: 150528 |
Author: 流云 |
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Description: 用比力导引法，计算某条件下算惯性器件在飞行期间内的敏感测量输出数值、导航输出数值(By using the method of specific force guidance, the sensitive measurement output value and the navigation output value of the inertial device during the flight are calculated.)
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Size: 1024 |
Author: Adonis4s |
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Description: 对近年来无人机飞行航迹算法做了技术分类和理论分析，希望对初学者有很好的指导作用(In recent years, UAV flight path algorithm has been classified and analyzed theoretically, hoping to have a good guidance for beginners.)
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Size: 16101376 |
Author: 会儿 |
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