結果
問題 |
No.654 Air E869120
|
ユーザー |
![]() |
提出日時 | 2025-03-31 17:42:43 |
言語 | PyPy3 (7.3.15) |
結果 |
AC
|
実行時間 | 149 ms / 2,000 ms |
コード長 | 3,021 bytes |
コンパイル時間 | 270 ms |
コンパイル使用メモリ | 82,220 KB |
実行使用メモリ | 87,184 KB |
最終ジャッジ日時 | 2025-03-31 17:43:41 |
合計ジャッジ時間 | 4,427 ms |
ジャッジサーバーID (参考情報) |
judge4 / judge5 |
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ファイルパターン | 結果 |
---|---|
sample | AC * 5 |
other | AC * 35 |
ソースコード
import sys from collections import deque class Edge: def __init__(self, to, rev, cap): self.to = to self.rev = rev self.cap = cap class Dinic: def __init__(self, n): self.size = n self.graph = [[] for _ in range(n)] def add_edge(self, fr, to, cap): forward = Edge(to, len(self.graph[to]), cap) backward = Edge(fr, len(self.graph[fr]), 0) self.graph[fr].append(forward) self.graph[to].append(backward) def bfs_level(self, s, t, level): q = deque([s]) level[:] = [-1]*self.size level[s] = 0 while q: v = q.popleft() if v == t: return for edge in self.graph[v]: if edge.cap > 0 and level[edge.to] == -1: level[edge.to] = level[v]+1 q.append(edge.to) def dfs_flow(self, v, t, upTo, iter_, level): if v == t: return upTo for i in range(iter_[v], len(self.graph[v])): edge = self.graph[v][i] if edge.cap > 0 and level[v] < level[edge.to]: d = self.dfs_flow(edge.to, t, min(upTo, edge.cap), iter_, level) if d > 0: edge.cap -= d self.graph[edge.to][edge.rev].cap += d return d iter_[v] += 1 return 0 def max_flow(self, s, t): flow = 0 level = [-1]*self.size while True: self.bfs_level(s, t, level) if level[t] == -1: return flow iter_ = [0]*self.size while True: f = self.dfs_flow(s, t, float('inf'), iter_, level) if f == 0: break flow += f level = [-1]*self.size def main(): input = sys.stdin.read().split() idx = 0 N = int(input[idx]); idx += 1 M = int(input[idx]); idx += 1 d = int(input[idx]); idx += 1 flights = [] for _ in range(M): u = int(input[idx]); idx += 1 v = int(input[idx]); idx += 1 p = int(input[idx]); idx += 1 q = int(input[idx]); idx += 1 w = int(input[idx]); idx += 1 flights.append((u, v, p, q, w)) size = 2 * M + 2 source = 2 * M sink = 2 * M + 1 dinic = Dinic(size) for i in range(M): u, v, p, q, w = flights[i] in_node = 2 * i out_node = 2 * i + 1 dinic.add_edge(in_node, out_node, w) if u == 1 and p >= 0: dinic.add_edge(source, in_node, 10**18) if v == N: dinic.add_edge(out_node, sink, 10**18) for i in range(M): _, v_i, _, q_i, _ = flights[i] for j in range(M): u_j, _, p_j, _, _ = flights[j] if i != j and v_i == u_j and (q_i + d) <= p_j: dinic.add_edge(2 * i + 1, 2 * j, 10**18) print(dinic.max_flow(source, sink)) if __name__ == '__main__': main()