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test.py

+import unittest
+import math
+from main import TAircraft, TMissle, RLS
+
+class testRLS(unittest.TestCase):
+
+    def test_Aircraft(self):
+
+        aircraft = TAircraft(9, 30, 15, math.pi/6)
+        aircraft.T0 = 0
+        aircraft.Move(10)
+        self.assertEqual(round(aircraft.x, 2), -12492.44)
+        self.assertEqual(round(aircraft .y, 2), -7187.71)
+
+    def test_Missle(self):
+        missle = TMissle(5, 10, 20, math.pi/6, 15)
+        missle.T0 = 0
+        missle.Move(0.1)
+        self.assertEqual(round(missle.x, 2), -174.19)
+        self.assertEqual(round(missle.y, 2), -93.45)
+
+    def testRlsPeleng(self):
+        air1 = TAircraft(200, 50, 50, math.pi / 3)
+        air2 = TAircraft(200, 60, 60, math.pi / 6)
+
+        mis1 = TMissle(1000, 10, -10, math.pi / 4, 30)
+        mis2 = TMissle(1000, 100, 150, math.pi / 4, 30)
+
+        Rls = RLS(50, 100, 1000)
+        Rls.Targets.append(air1)
+        Rls.Targets.append(air2)
+        Rls.Targets.append(mis1)
+        Rls.Targets.append(mis2)
+        Rls.Peleng(0, 10, 0.1)
+
+        f = open('log.txt')
+        lines = []
+        for line in f:
+            lines.append(line)
+        f.close()
+        true_lines = ['0.1; Aircraft #1; D = 475.42512792323026; Az = 1.2782078793302332\n',
+ '0.1; Aircraft #2; D = 480.19721022253833; Az = 0.687805100917794\n',
+ '0.1; Missle #1; D = 998.5335823515045; Az = -0.044676900377693035\n',
+ '0.2; Aircraft #1; D = 943.465660043936; Az = 1.1634512982485217\n',
+ '0.3; Missle #1; D = 972.9064248219566; Az = -0.07545850062851994\n',
+ '0.4; Missle #1; D = 907.1337221989091; Az = -0.16918781005900826\n',
+ '0.5; Missle #1; D = 822.114416066153; Az = -0.3423586811055799\n',
+ '0.6; Missle #1; D = 749.778746706199; Az = -0.6283903712185259\n',
+ '0.7; Missle #1; D = 747.3045172925204; Az = -1.0212847158511866\n',
+ '0.8; Missle #1; D = 872.6102282527802; Az = -1.410419725639589\n']
+        self.assertEqual(lines, true_lines)
+
+
+print('All tests passed correctly!')
+
+