搜索资源列表
SAR-satellites
- 利用SAR卫星在多个时刻的位置和速度信息，计算出任意象元成像时刻卫星的位置，拟合出SAR卫星的轨道模型。-Using SAR satellite in multiple time position and velocity information to calculate as the image element imaging time satellite position, fitting the SAR satellite orbital model.
astrogator
- 属于stk二次开发，通过matlab调用stk中astrogator模块，实现轨道转移-Belonging to the stk secondary development, matlab call stk in the astrogator module, orbital transfer
shiyan
- 其中nadate和naname是小行星的名称和轨道根数-Of which nadate and naname the name of the asteroid and the orbital elements
naname
- 轨道根数和位置的转换 naname和nadata是行星的名字和轨道根数-The the conversion naname nadata of the orbital elements and the location is the name of the planet' s orbital elements
sv_from_coe
- 把轨道根数转移到对应的状态向量，在轨道中很常用。-The orbital elements are transferred to the state vector
coe_from_sv
- 有卫星状态向量转移至轨道根数，在轨道计算中很常用。-The transfer of the satellite state vector to the orbital elements is very commonly used in orbital calculations.
lambert
- 求解Lambert问题。 输入：轨道上两个点的位矢R1、R2，以及从R1到R2所用的时间t(缺点是脉冲太大)。 输出：质点在R1端点的速度V1，质点在R2端点的速度V2. 此函数用于：在给定轨道上两个点的位矢R1、R2，以及从R1到R2所用的时间t。求解V1、V2。再调用前面的函数就可以确定轨道根数，及任意时刻质点的状态。-To solve the Lambert problem. Input: track two-point position vector R1, R
KSolveKeplerEe
- 开普勒方程求解函数, 方便简单，，空间飞行器轨道计算常用 -Kepler equation solver function, convenient and simple, commonly used in space vehicle orbital calculations
coe_from_sv
- 将状态矢量转换成轨道根数的Matlab源程序，输入是位置速度矢量，输出是轨道根数，有详细的注解-Convert the state vector of the orbital elements of the Matlab source code, enter the location of the velocity vector, the output of the orbital elements, with detailed comments
cppOrbitTools
- 轨道计算小程序，封装多个预报模型，包括SGP4/SDP4模型，同时附一个例子代码-Orbital calculation program package multiple forecasting model, including SGP4/SDP4 model, while attached to an example of code
track-count-and--ephemeris-count
- 运用给出的相关参数，设计一种巧妙计算出轨道参数及反算卫星星历的算法-Use of the given parameters, design an ingenious algorithm calculate the orbital parameters and Inverse satellite ephemeris
Prange
- 根据广播星历文件画出轨道，GPS卫星定位与导航课上的作业。-Orbital to jobs on the GPS satellite positioning and navigation courses based on broadcast ephemeris file.
optimal_impulsive
- 最优脉冲轨道机动所需的圆形或椭圆形地球轨道的航天器。optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit-Round or oval Earth orbit spacecraft the optimal pulse orbital maneuvering required. optimal impulsive maneuver required to
solar
- 绘制太阳系行星，以及行星轨道，轨道椭圆，有倾斜，功能-Draw the planets in our solar system and planetary orbits, orbital ellipse, tilt function
main1
- 数学建模中模拟卫星轨道的matlab源程序，由仿真数据模拟卫星轨道方程中的参数，得到轨道方程。-Matlab source, by mathematical modeling to simulate the satellite orbit parameters in the simulation data analog satellite orbit equation, the orbital equation.
PA1100
- PA1100磁头解码芯片驱动代码，支持银行卡轨道1、2、3数据，支持正反向刷卡，执行结果分别打印出磁条卡的3个轨道数据。-PA1100 head decoder chip driver code, support bank card orbital 1,2,3 data support the pros and cons to the credit card, the results of the implementation were to print out the magnetic str
PA1100headerdecoderSourcCode.r
- PA1100磁头解码芯片源代码。PA1100磁头解码芯片驱动代码，支持银行卡轨道1、2、3数据，支持正反向刷卡，执行结果分别打印出磁条卡的3个轨道数据,The PA1100 head decoder chip source code. PA1100 head decoder chip drive code, support bank card orbital 1,2,3 data support the pros and cons to the credit card, the results
ghost-imaging
- 利用双光子纠缠方法进行双路轨道角动量光学鬼成像过程。-Using two-photon entanglement the dual orbital angular momentum of optical ghost imaging process.
test-ghost-simulation
- 利用轨道角动量纠缠态进行双路相关鬼成像，测试性能。-Orbital angular momentum entanglement in a dual ghost imaging, test performance.
sunsnchronous
- 太阳同步卫星及其轨道计算，用于设计太阳同步轨道，并且给出一个实例，介绍卫星轨道参数的计算方法-Sun-synchronous satellites and their orbital calculations for the design of a sun-synchronous orbit, and an example is given, satellite orbit parameters calculation method