結果

問題 No.654 Air E869120
ユーザー lam6er
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
このコードへのチャレンジ
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ファイルパターン 結果
sample AC * 5
other AC * 35
権限があれば一括ダウンロードができます

ソースコード

diff #
プレゼンテーションモードにする

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()
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