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Skyline
- 路线转移功能，可以通过鼠标画一个转移的路线，双击鼠标结束画线。创建好路线之后， 再创建一个动态对象，动态对象以之前创建好的路线作为运动的轨迹-Line transfer function, you can transfer the mouse to draw a line, double-click the mouse to draw a line end. Created routes, Then create a dynamic object, dynamic objects to
wind_jianmo_fangzhen
- 从风场的统计特性出发，建立了适用于弹道计算的简化风场模型。以这些模型为基础进行了弹道计 算.模拟了不同风场模型引起的弹箭射击误差，揭示了风与弹道误差的对应关系.为风修正弹箭设计提供了参考依据。 -Congfeng statistical properties of the starting field, the establishment of ballistics applicable to the simplified calculation of the wind field mo
MATLAB_Simulink_dandaofangzhen_mokuai
- 用Simulink工具箱,对导弹仿真模型进行了模块化设计,条理清晰,信息流流向明确,具有很好 的可视化效果,增加了模块的可移植性。最后在一定条件下仿真得出了弹道及部分参数的变化结果,结果已经得到初步验证。 -Using Simulink toolbox, the missile simulation model modular design, the clarity of the information flow the flow of clear, with good visualiz
Matlab_3dof_animation
- 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
aircraft_trajectory_simulation
- 对某飞行器的全空域飞行弹道进行了仿真研究.建立了飞行器空间运动的数学模型，应用“牛顿插值多项式法”对气动力参数进行了辨识，用C语言编制了仿真程序，并给出了仿真结果及分析。-Of a vehicle-wide airspace simulation trajectory. Established the aircraft mathematical model of space motion, application, Newton interpolation polynomial method
GA_missile_trajectory_simulation
- 提出了一种空面导弹下滑段、俯冲攻击段的弹道优化设计方案,以及一 种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制 方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总 体设计参数的目的。 -A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a cou
real_time_simulaion_outer_trajectory_simulation.ra
- 实时仿真系统中关于坦克炮炮弹外弹道仿真方法还不成熟，该文在分析了现有几种方法 优缺点的基础上，提出基于射表的抛物线拟合方法，并给出了程序流程图以及几种拟合曲线方程。 通过实际应用证明这种方法运算简便、快捷，可以满足实时仿真的要求，而且可以推广到装甲步兵战车等类似系统上使用。 -Real-time simulation system on the tanks, artillery shells outside the trajectory simulation methods are
trajectory3
- Trajectory and Attitude Plot This function plot in the same figure the center trajectory and attitude of an aircraft.
AdvancesinLinear
- SIAM s Advances in Design and Control series consists of texts and monographs dealing with all areas of design and control and their applications. Topics of interest include shape optimization, multidisciplinary design, trajectory optimization, f
matlab-trajectory
- 铅垂平面飞行弹道设计，仿真分析与实验报告，内附了源程序代码-Vertical plane trajectory design, simulation and experimental reports included the source code
trajectory-optimization
- 针对登月舱上升段轨迹优化问题，建立上升舱动力学模型，用无量纲技术建立最优控制模型；以燃料消耗最优为指标，利用Pontrjagin极小值原理，将问题转化为时间自由的两点边值问题(TPBVP)。采用一种基于初值猜测方法和向前扫描法求解TPBVP，得到最优上升轨迹。仿真结果表明：此方法收敛速度快、可靠性高，为月面返回实际应用提供一定的参考。-According to the problem of trajectory optimization for the lunar module in ascen
trajectory-generation
- 为了在轨迹规划阶段提高月球车在三维地形中的轨迹规划精度，以被动关节式地形自适应月球车为研 究对象，融合关节机器人D-H 坐标建模方法构建月球车悬架运动学模型，结合数值求解方法，推导了任意崎岖 三维地形中月球车姿态估计模型。在模型估计基础上利用参数化控制原理，建立了满足约束条件下被动关节式 月球车在任意地形中的基于模型估计的一般性参数化轨迹生成模型。针对轮式月球车的非完整性特点，结合数 值求解方法，推导了非线性模型的求解方法。最后利用仿真方法，以八轮摇杆摇臂关节式月球车为例，验证了
ADVANCED-MOUSE-POINTER-CONTROL-USING-TRAJECTORY.r
- ADVANCED MOUSE POINTER CONTROL USING TRAJECTORY
Design-of-a-Nonlinear-PID-Neural-Trajectory-Track
- Design of a Nonlinear PID Neural Trajectory Tracking Controller for Mobile Robot based on Optimization Algorithm
spatio-temporal-trajectory
- Travel feature mining method based on spatio-temporal trajectory data
trajectory-clustering
- Computation of spatio-temporal trajectory clustering method
Trajectory-Shape-Varying-Missile-Guidance-for-Int
- Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles during the Boost Phase
The-Systematic-Trajectory-Search-Algorithm-for-Fe
- In this paper we present the systematic trajectory search algorithm (STSA) which first globally explores the solution space then makes thorough local searches in promising areas. The STSA has been tested on training feedforward neural network
Trajectory-Simulation
- 基于Matlab的比例导引弹道仿真分析.介绍了比例导引法的导引规律, 推导了基于比例导引规律的拦截弹弹道方程-Trajectory Simulation Analysis Based on Matlab
airship-trajectory-tracking
- 研究了在系统存在不确定性或外界干扰的情况下飞艇的三维航迹控制问题-The three-dimensional trajectory control problem for an airship with parameter uncertainties and external disturbances was considered.