代码搜索：海事卫星

找到约 406 项符合「海事卫星」的源代码

代码结果 406
热门代码： main.c GPIO I2C SPI UART timer interrupt ADC PWM LED
www.eeworm.com/read/322126/13389526

c tranf.c

tranf.c double zenith1(xj,yj,zj,xi,yi,zi) double xj,yj,zj,xi,yi,zi; /* 利用卫星坐标xj, yj, zj和测站坐标xi, yi, zi 计算卫星j相对于测站i的天顶距离 */ { double fi,lambda,h,pji,z,Ae=0.,FLAT=0.; pji = sqrt((xj-
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www.eeworm.com/read/482300/6622495

c tranf.c

tranf.c double zenith1(xj,yj,zj,xi,yi,zi) double xj,yj,zj,xi,yi,zi; /* 利用卫星坐标xj, yj, zj和测站坐标xi, yi, zi 计算卫星j相对于测站i的天顶距离 */ { double fi,lambda,h,pji,z,Ae=0.,FLAT=0.; pji = sqrt((xj-
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www.eeworm.com/read/250696/12388553

c tranf.c

tranf.c double zenith1(xj,yj,zj,xi,yi,zi) double xj,yj,zj,xi,yi,zi; /* 利用卫星坐标xj, yj, zj和测站坐标xi, yi, zi 计算卫星j相对于测站i的天顶距离 */ { double fi,lambda,h,pji,z,Ae=0.,FLAT=0.; pji = sqrt((xj-
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www.eeworm.com/read/227760/14413877

c tranf.c

tranf.c double zenith1(xj,yj,zj,xi,yi,zi) double xj,yj,zj,xi,yi,zi; /* 利用卫星坐标xj, yj, zj和测站坐标xi, yi, zi 计算卫星j相对于测站i的天顶距离 */ { double fi,lambda,h,pji,z,Ae=0.,FLAT=0.; pji = sqrt((xj-
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www.eeworm.com/read/248882/12536132

c tranf.c

tranf.c double zenith1(xj,yj,zj,xi,yi,zi) double xj,yj,zj,xi,yi,zi; /* 利用卫星坐标xj, yj, zj和测站坐标xi, yi, zi 计算卫星j相对于测站i的天顶距离 */ { double fi,lambda,h,pji,z,Ae=0.,FLAT=0.; pji = sqrt((xj-
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www.eeworm.com/read/436367/7771029

cpp yanjun.cpp

#include #include #include /*********************************************************1*/ struct GPS01 //卫星结构体 { int tai; //状态 int
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www.eeworm.com/read/145151/12749206

++

VERSION 5.00 Begin VB.Form Form1 AutoRedraw = -1 'True BackColor = &H00000000& BorderStyle = 1 'Fixed Single Caption = "卫星轨道" ClientHeight =
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www.eeworm.com/read/231676/14224069

sql ufotab.sql

create table ufotab(sname varchar(50) not null, 卫星经度 float(10) not null, primary key(sname)); insert into ufotab values('雅玛尔202' , '49.0'); inse
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www.eeworm.com/read/140414/13083031

m compsatpos.m

function R = CompSatpos(omeg0,M0,t) %利用星历计算卫星的位置 %omeg0 初始升交点赤经 %Mo %t 计算卫星位置的时刻 a = 26609000; i = 55*pi/180; n0 = 30.085*pi/180/3600; wie = 15*pi/180/3600; t0=0; omeg0 = omeg0*pi/180;
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www.eeworm.com/read/140414/13083033

m compsatvel.m

function V = CompSatvel(omeg0,M0,t) %利用星历计算卫星的速度 %omeg0 初始升交点赤经 %Mo %t 计算卫星速度的时刻 a = 26609000; i = 55*pi/180; n0 = 30.085*pi/180/3600; wie = 15*pi/180/3600; t0=0; omeg0 = omeg0*pi/180;
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