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.
Ex4-22 單射函數問題
« 問題描述：
設函數f將點集S = {0,1, , n -1}映射為f (S) = { f (i) | iÎ S} Í S 。單射函數問題要
從S中選取最大子集X Í S 使f (X )是單射函數。
例如，當n=7， f (S) = {1,0,0,2,2,3,6} Í S 時， X = {0,1,6} Í S 是所求的最大子集。
« 編程任務：
對于給定的點集S = {0,1, , n -1}上函數f，試用抽象數據類型隊列，設計一個O(n)時
間算法，計算f的最大單射子集。
« 數據輸入：
由文件input.txt 提供輸入數據。文件的第1 行有1 個正整數n，表示給定的點集
S = {0,1, , n -1}。第2 行是f (i)的值，0 £ i < n。
« 結果輸出:
程序運行結束時，將計算出的f的最大單射子集的大小輸出到output.txt中。
輸入文件示例 輸出文件示例
input.txt
7
1 0 0 2 2 3 6
output.txt
3
