搜索资源列表
guidao
- 关于空间目标轨道确定专家系统的小论文，很有帮助-target orbit on space expert system to determine the small papers, helpful
rtklib_2.4.1 卫星数据解算的程序
- rtklib 版本2.4.1 An Open Source Program Package for GNSS Positioning 日本开源网站上提供的关于卫星数据解算的程序。All of the executable binary APs for Windows are included in the package as well as whole source programs of the library and the APs. * For real-time PP
weixinguidaoliugenshu
- 卫星轨道六根数，基本公式和基本理论-Satellite orbit six numbers, the basic formula and basic theory. . . . . . . . .
missile
- 空地导弹全弹道仿真建模(说明文件)：自由下滑段+固定倾角下滑+转平飞过渡段+平飞段+导引段-missile simulation/matlab
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
satellite_orbit
- source code of sat orbit
TDAPR_oddyn
- The dynamics of orbit uncertainty in an unstable orbital environment are discussed with specific application to the orbit determination of a halo orbit about the Earth{Sun L1 point. This article documents a simplified orbit determination covari
SATELLITEORBIT
- This paper discusses the establishment and relevant accomplishments of a simple facility used for students learning aids based on the Keplerian Orbit parameters. Three major areas in Orbital Mechanics are discussed in this paper, Orbit of a satel
SpaceFlightDynamics
- The ballistic category of atmospheric vehicles includes missiles, launch ve- hicles, and entry capsules. Some missiles and launch vehicles incorporate fi ns as aerodynamic stabilizing and control surfaces. The spacecraft are also catego-
xlptanh
- Spatial registration of multidate or multisensor images is required for many applications in remote sensing, such as change detection, the construction of image mosaics, DEM generation from stereo pairs, and orthorectifi cation. Registration
elfind.5
- Creates a TLE from two or three observations of a satellite on a single pass. Useful for initial orbit parameters and for unknown satellite identification. This fifth version improves convergence characteristics for the three point fit via F and G se
weixingdinggui
- 卫星定轨，研究卫星间的距离以及相对的角度，有需要的同学可以看看啊，很有帮助-Satellite orbit to study the distance between the satellite and the relative point of view, students need to take a look, ah, very helpful
GPS
- 究了适用于低轨卫星的Doppler-Range联合定位法及TDOA-TDOF联合定位法。分析了联合定位的误差计算公式，并提出了一种衡量联合定位性能的参数。 -Study of low-orbit satellites for the Doppler-Range joint positioning method and TDOA-TDOF joint positioning method. Analysis of the joint positioning error formula, and
orbit
- 轨道摄动力电子书，供大家参考 讲得比较简明扼要-Orbital perturbation power book, put it more concise for your reference
satelite-obit
- 这是中科院研究生院课程课件，电子所所开的，主要讲的是卫星轨道的内容，希望对大家有帮助-This is the Graduate School of Chinese Academy of Sciences Courseware, e are the open, mainly about the content of the satellite orbit, we hope to help
CSliderCtrl
- 滑动条控制（Slider Control）也叫轨道条控制，其主要是用一个带有轨道和滑标的小窗口以及窗口上的刻度，来让用户选择一个离散数据或一个连续的数值区间。通过鼠标或键盘来进行数据的选择操作，这在WIN98/95中的很多应用程序中都可以看到，如控制面板中的鼠标等，滑动条既可以是水平方式的也可以是垂直方式的。-The slider control (Slider Control) is also called the orbit control, its main use with a trac
GNSS-Orbit-and
- 卫星轨道钟差卡尔曼修正-国外导航年会ION2011的文章，网络下载需要$25，-Real-time Combination of GNSS Orbit and Clock Correction Streams Using a Kalman Filter Approach
A Tracking Approach for Inclined Orbit Satellites
- An approach to track satellites that are in inclined orbits. Fusion of 2 types of estimators.
axis-orbit
- 本模型是计算轴心轨迹的理论模型，主要功能是进行轴心轨迹计算。-here is a modle of axis orbit,The main fuction is to calculate axis shaft orbit.
orbital mechanics
- Orbit mechanics for enginnering students