代码搜索：initial
找到约 10,000 项符合「initial」的源代码
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www.eeworm.com/read/287166/8713756
h searchp.h
// Emacs style mode select -*- C++ -*-
//-----------------------------------------------------------------------------
//
// $Id: searchp.h,v 1.1 2000/08/21 21:17:32 metzgermeister Exp $
//
// Copy
www.eeworm.com/read/287166/8713759
c dosstr.c
// Emacs style mode select -*- C++ -*-
//-----------------------------------------------------------------------------
//
// $Id: dosstr.c,v 1.2 2000/09/10 10:53:46 metzgermeister Exp $
//
// Copyr
www.eeworm.com/read/287166/8714363
changelog
/* $Id: ChangeLog,v 1.3 2001/03/31 10:14:09 ydario Exp $ */
2001-03-21: Yuri Dario
- pause game when losing focus
- print messages when changing window size
2001-03-04:
www.eeworm.com/read/287060/8728612
c 数据结构3.c
#include
void main()
{
struct childrec/*定义结构体*/
{
char initial; /* 姓名首字母 */
int age; /* 年龄 */
int grade; /* 考试成绩 */
}boy,girl;
www.eeworm.com/read/430470/8744076
m rk_wjl.m
function [x,y]=rk_wjl(odefile,xi,xf,yi,h,varargin)
x = [xi:h:xf]; % Vector of x values
if x(end) ~= xf
x(end+1) = xf;
end
y(1) = yi; % Initial condition
d = diff(x);
% if no this sen
www.eeworm.com/read/286578/8758091
h liststudent.h
#ifndef LISTSTUDENT_H_
#define LISTSTUDENT_H_
#include
#include "linkstudent.h"
using namespace std;
class Liststudent
{
private:
Linkstudent *first;
Linkstudent *tail;
int si
www.eeworm.com/read/386253/8759939
m alg054.m
% ADAMS-FOURTH ORDER PREDICTOR-CORRECTOR ALGORITHM 5.4
%
% To approximate the solution of the initial value problem
% y' = f(t,y), a
www.eeworm.com/read/386253/8760126
m alg054.m
% ADAMS-FOURTH ORDER PREDICTOR-CORRECTOR ALGORITHM 5.4
%
% To approximate the solution of the initial value problem
% y' = f(t,y), a
www.eeworm.com/read/429621/8798382
m m3.m
% M-file for Exercise 3 RL circuit simulation
% input parameters and initial conditions
R = 0.4; %R = 0.4 ohm
L = 0.04; %L = 0.04 Henry
we = 314; % excitation frequency in rad/sec
Vac_mag =
www.eeworm.com/read/429246/8814162
m initialparameters.m
%Initial values of the constants are given
g = 32.2; % Acceleration due to gravity (ft/sec^2)
tauc = 5; % Correlation time of aircraft vertical acceleration
tauT = 4; % Correlation time of