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missile_guidance
- 导弹制导算法MATLAB仿真例程，制导系统、自寻的制导律设计与仿真，如追踪法、平行接近法、比例导引法等-Missile guidance algorithm based on MATLAB simulation routines, guidance systems, guidance law design and simulation of self-seeking, such as tracing, nearly parallel method, proportional navigation
GPSsignalgeneration
- 利用Matlab生成GPS C/A 码的基带信号。 （1）产生卫星PRN 号码为“5”的一组C/A 码； （2）循环生成25 页的导航数据，GPS 时间可填入一固定的已知数值； （3）生成C/A 码扩频信号，每个C/A 码码片给出4 个采样数据； （4）基带信号采用方波信号，电平为0 和1，占空比为50 ％， 不加入噪声，进一步生成某个特定的中频信号-The baseband signal is generated using Matlab GPS C/A code.
Saeed
- it`s a matlab code about navigation in ecef cordination
code_matlab
- 惯性导航加速度计标定误差计算matlab程序-Inertial navigation Accelerometer Calibration error calculation matlab program
GPS
- GPS卫星导航定位的算法，包括码生成，载波生成，和导航解算等matlab算法-GPS satellite navigation and positioning algorithms, including code generation, carrier generation, and navigation algorithm matlab solver, etc.
GPS-positioning-
- 用MATLAB程序实现卫星位置解算、用户位置解算（最小二乘法）、导航电文读取、坐标转换。-MATLAB program to achieve the satellite position solver, solver user location, navigation message reads, GPS positioning simulation (implemented by the least squares method).
Missile-algorithm
- 基于MATLAB导弹仿真源代码(missile simulation) 给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Missile simulation based on MATLAB source code (missile simulation) Differential equation gives the proportiona
atti_cal
- 惯性导航程序，matlab编辑，旋转矢量法结合方向余弦矩阵，完美计算姿态阵，惯导姿态更新程序-Inertial navigation procedures, matlab editing, rotation vector direction cosine matrix method combined with perfect posture matrix calculation, INS attitude update
geonav_NED
- This matlab code is for navigation simulation in geographical NED coordinate system which gives position and attitude of a IMU system.
GNT08.1.2
- GPS导航 无线电导航 位置偏差校正 MATLAB仿真-This program include Principle of Radio Navigation Calculation and GPS position error corrections.
gps2ins
- INS-GPS 惯性-天文组合导航 这个导航算法基于MATLAB环境，需要有惯性、天文的测量数据，最后结果是三个姿态角，以及一些误差信息。-Inertia- Astro Navigation I completed my graduation this design so that
bilidaoyinfa
- 反直升机导弹采用比例导引法攻击目标直升机 导弹发射位置：(0,0) 导弹速度：500m/s 直升机速度：100m/s 直升机爬升角度： 8° 直升机初始位置（四个）： （4000,1000）、（4000，-1000） （4000,100 ）、（4000,-100） 比例导引律k=1.5（可以自行在程序中修改）-this matlab program is aimed to simulate the track of the anti-helicopter miss
dandaofangzhen
- matlab/simulink 三种方法的弹道仿真（追踪法、比例导引法、平行接近法） -matlab/simulink Trajectory Simulation of three methods (tracing method, proportional navigation law, parallel close to the law)
455465
- 应用GPS与SINS进行的组和导航问题 基于matlab编程-Groups and GPS navigation application issues and conducted SINS
LSPzuhe14_8
- 多星座导航系统中利用最小二乘算法进行位置解算的MATLAB傆代码，以GPS/GLONASS系统为例-Multi-constellation navigation system using least square algorithm solver of MATLAB Yuan location code to GPS/GLONASS system as an example
jat-code-968-trunk
- 用于解决航天动力学，航天任务设计，导航制导控制问题-The Java Astrodynamics Toolkit is a library of components to help users create their own application programs to solve problems in astrodynamics, mission design, spacecraft navigation, guidance and control using Java or Matl
eetop.cn_GPSL1_SoftReceiver_MATLAB
- GPS信号MATLAB捕获跟踪程序，对于搞卫星导航接收机方向的同学很有用-MATLAB GPS signal acquisition and tracking procedures for working in the satellite navigation receiver students useful direction
AutonomousNavigation
- 利用matlab仿真汽车的泊车过程，利用GUI搭建汽车自动泊车系统，实现汽车导航与泊车-Using MATLAB to simulate the parking process of the car, using GUI to build auto parking system, realize the car navigation and parking.
INS
- Matlab Simulation of Strapdown Inertial Navigation System (INS) of circular trajectory,with the specific force and angular velocitie document text -Matlab Simulation of Strapdown Inertial Navigation System (INS) of circular trajectory,with the s
Desktop
- matlab simulation to generate circular trajectory ,and solving his specific force and angular velocitie for inertial navigation system-matlab simulation to generate circular trajectory ,and solving his specific force and angular velocitie for inertia