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qianzhiliangfa
- 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
sandianfa
- 三点法弹道仿真。三点法导引是指导弹在攻击目标过程中始终位于目标和制导站的连线上的一种导引方法。通过建模仿真，使大家更形象生动的理解三点法。-Trajectory Simulation of the three-point method. The three-point method guide refers to the guided missile targets is always in the process of a guide on the objectives and guidanc
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
navigation-yan
- 严老师编写的惯性/GPS组合导航相关程序，包括轨迹生成、滤波、解算等-Inertial/GPS navigation strict teacher written procedures, including trajectory generation, filtering solver
Trajectory-Program
- 本程序为风干扰下弹道解算程序，包括matlab程序和simulink程序，非常实用-The procedures for the wind interference under ballistic solver, including the the matlab procedure and simulink program, very useful
3ddandao
- 3D弹道仿真VC程序以及源代码文件，外弹道经典的解三自由度弹道方程，运行结果将显示：落地误差、飞行时间、修正射程、侧偏等参数。用C语言编写，程序注释丰富，运行时请把Debug目录中的EXE文件拷贝至根目录中运行，否则出错。-3D trajectory simulation VC program and source code files, the solution of three classic exterior ballistics degree trajectory equation, t
Missile-Fly
- 导弹飞行轨迹的数值模拟程序（已知初始位置及状态），考虑了科氏力和地球自转的影响，比较实用。-Numerical simulation of the missile trajectory program (known initial position and status), taking into account the Coriolis force and the Earth s rotation, more practical.
Asynchronous_motor_subdivision
- 传统异步电机直接转矩控制多采用六边形磁链控制或六区间的圆形磁链控制，容易造 成转矩和磁链脉动过大，限制了其实用范围。针对此缺陷，本文采用矢量细分的方法，将传统的六电压矢量和六扇区细分为十二电压矢量和十二个扇区，制定了相应的矢量开关表，并通过 MATLAB 对其进行了仿真实验。仿真结果表明，基于矢量细分的异步电机直接转矩控制能够有效改善磁链轨迹，减小转矩脉动，提高系统控制性能。 -Conventional induction motor direct torque control multip
hybrid_pseudo_L
- 高超声速飞行器上升轨迹优化计算。采用勒让德伪谱法直接优化方法。-trajectory optimization of hypersonic craft program with legendre method
SINS_simulation
- 基于MATLAB的捷联惯导轨迹发生器，以及SINS解算程序-SINS based on MATLAB trajectory generator and solver SINS
dandao2
- 大气中的火箭弹道模拟，考虑空气阻力因素，用4阶龙格库塔解运动方程-Atmospheric rocket trajectory simulation, considering air resistance factor, with fourth-order Runge-Kutta solution of the equations of motion
Kalman_filter
- 建立雷达对目标的跟踪算法，并进行仿真分析，给出仿真结果，画出目标真实轨迹、对目标的观察和滤波曲线。-Establishment of radar target tracking algorithm and simulation analysis, simulation results, draw real target trajectory, the target of observation and filter curves.
Cop
- 计算cop 轨迹，图片展示cop，以及时间轴展示三维cop-Calculated cop trajectory Photo Gallery cop, as well as the timeline shows a three-dimensional cop
fangzheng0
- 该程序是对飞行器的航迹进行模拟。包括3个文件，主程序是fangzhen.m，可以反映出飞行器高度、速度、攻角等参数对飞行器航迹的有效-The program is a simulated aircraft track. Includes three files, the main program is fangzhen.m, can reflect the aircraft altitude, speed, angle of attack of the aircraft trajectory p
NURBS-shishidongtaichabu
- 在数控加工中，采用NURBS插补算法，这是轨迹的仿真，并可以进行精度的分析-In CNC machining, using NURBS interpolation algorithm, which is the simulation trajectory and accuracy can be analyzed
daodanfeixinglixue
- 通过导弹的空气动力系数计算导弹的之心运动方程组，并利用MATLAB进行绘图，包括轨迹，速度时间曲线等-Aerodynamic coefficients calculated by missile missile equations of motion of the heart, and using MATLAB graphics, including trajectory, velocity-time curve
missileg
- 轨迹发生器，包含助推段，加速段，巡航段，下降段及落地，大机动，高空高速。完全正确。-Trajectory generator, including the boost phase, the acceleration, cruise segment, down section and landing, large motor, high-altitude high speed. Entirely correct.
ENEAP
- ENEA太陽運行軌跡公式MATLAB source code-ENEA sun trajectory equations MATLAB source code
MinEnergeOrbit
- 可生成从任意点发射攻击全球任意点的一条最小能量弹道，并确定关机点参数。-Can generate a minimum energy trajectory launch attacks from any point to any point worldwide, and to determine the shutdown point parameters.
ykddfz
- 利用MATLAB进行铅垂平面有控弹道仿真，并给出参数结果-Vertical plane with MATLAB simulation of controlled trajectory, and the results are given parameters