/*
* EULER S ALGORITHM 5.1
*
* TO APPROXIMATE THE SOLUTION OF THE INITIAL VALUE PROBLEM:
* Y = F(T,Y), A<=T<=B, Y(A) = ALPHA,
* AT N+1 EQUALLY SPACED POINTS IN THE INTERVAL [A,B].
*
* INPUT: ENDPOINTS A,B INITIAL CONDITION ALPHA INTEGER N.
*
* OUTPUT: APPROXIMATION W TO Y AT THE (N+1) VALUES OF T.
*/
Procedure TSPSA:
begin
init-of-T { T為初始溫度}
S={1，……，n} {S為初始值}
termination=false
while termination=false
begin
for i=1 to L do
begin
generate(S′form S) { 從當(dāng)前回路S產(chǎn)生新回路S′}
Δt:=f(S′))-f(S) {f(S)為路徑總長}
IF(Δt<0) OR (EXP(-Δt/T)>Random-of-[0,1])
S=S′
IF the-halt-condition-is-TRUE THEN
termination=true
End
T_lower
End
End
結(jié)合單片機(jī)和M a t l a b 兩者的優(yōu)點(diǎn)，基于事件驅(qū)動的中斷通信機(jī)制，提出一種Matlab 環(huán)境下PC 機(jī)與
單片機(jī)實(shí)時(shí)串行通信及數(shù)據(jù)處理的方法；完成單片機(jī)數(shù)據(jù)采集系統(tǒng)與PC 機(jī)的RS-232/RS-485 串行通
信及其通信數(shù)據(jù)的分析處理、文件存儲、F I R 濾波及圖形顯示；簡化系統(tǒng)開發(fā)流程，提高開發(fā)效率。
該方法已成功應(yīng)用于一個(gè)P I C 1 6 F 8 7 6 單片機(jī)應(yīng)用系統(tǒng)實(shí)例之中
f your application uses MFC in a shared DLL, and your application is
in a language other than the operating system s current language, you
will need to copy the corresponding localized resources MFC42XXX.DLL
from the Microsoft Visual C++ CD-ROM onto the system or system32 directory,
and rename it to be MFCLOC.DLL. ("XXX" stands for the language abbreviation.
For example, MFC42DEU.DLL contains resources translated to German.) If you
don t do this, some of the UI elements of your application will remain in the
language of the operating system.
實(shí)現(xiàn)最優(yōu)二叉樹的構(gòu)造；在此基礎(chǔ)上完成哈夫曼編碼器與譯碼器。 假設(shè)報(bào)文中只會出現(xiàn)如下表所示的字符：
字符 A B C D E F G H I J K L M N
頻度 186 64 13 22 32 103 21 15 47 57 1 5 32 20 57
字符 O P Q R S T U V W X Y Z ， ．
頻度 63 15 1 48 51 80 23 8 18 1 16 1 6 2
要求完成的系統(tǒng)應(yīng)具備如下的功能：
1．初始化。從終端（文件）讀入字符集的數(shù)據(jù)信息，。建立哈夫曼樹。
2．編碼：利用已建好的哈夫曼樹對明文文件進(jìn)行編碼，并存入目標(biāo)文件（哈夫曼碼文件）。
3．譯碼：利用已建好的哈夫曼樹對目標(biāo)文件（哈夫曼碼文件）進(jìn)行編碼，并存入指定的明文文件。
4．輸出哈夫曼編碼文件：輸出每一個(gè)字符的哈夫曼編碼。
This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear
approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot s
stick pitch command as the set point for the aircraft s pitch attitude and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system.
