mirror of https://github.com/ArduPilot/ardupilot
autotest: add test for loiter-to-alt
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QGC WPL 110
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0 0 0 16 0.000000 0.000000 0.000000 0.000000 -27.274439 151.290064 343.100006 1
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1 0 3 84 0.000000 0.000000 0.000000 0.000000 -27.272768 151.288529 30.000000 1
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2 0 3 16 0.000000 0.000000 0.000000 0.000000 -27.273631 151.289380 30.000000 1
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3 0 3 31 0.000000 0.000000 0.000000 0.000000 -27.275714 151.291065 120.000000 1
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4 0 3 17 0.000000 0.000000 0.000000 0.000000 -27.278535 151.298429 120.000000 1
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5 0 3 31 0.000000 -100.000000 0.000000 0.000000 -27.277746 151.298205 50.000000 1
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6 0 3 16 0.000000 0.000000 0.000000 0.000000 -27.274219 151.294322 40.000000 1
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7 0 3 16 0.000000 0.000000 0.000000 0.000000 -27.273160 151.290969 30.000000 1
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8 0 3 85 0.000000 0.000000 0.000000 0.000000 -27.272804 151.288573 0.000000 1
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@ -933,6 +933,22 @@ class AutoTestQuadPlane(AutoTest):
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self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, -1)
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self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, -1)
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self.disarm_vehicle()
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self.disarm_vehicle()
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def MAV_CMD_NAV_LOITER_TO_ALT(self, target_system=1, target_component=1):
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'''ensure consecutive loiter to alts work'''
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self.load_mission('mission.txt')
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self.change_mode('AUTO')
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self.wait_ready_to_arm()
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self.arm_vehicle()
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self.wait_current_waypoint(4, timeout=240)
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self.assert_altitude(120, accuracy=5, relative=True)
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self.delay_sim_time(30)
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self.assert_altitude(120, accuracy=5, relative=True)
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self.set_current_waypoint(5)
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self.wait_altitude(altitude_min=65, altitude_max=75, relative=True)
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if self.current_waypoint() != 5:
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raise NotAchievedException("Should pass 90m before passing waypoint 5")
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self.wait_disarmed(timeout=300)
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def Mission(self):
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def Mission(self):
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'''fly the OBC 2016 mission in Dalby'''
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'''fly the OBC 2016 mission in Dalby'''
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self.fly_mission(
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self.fly_mission(
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@ -962,5 +978,6 @@ class AutoTestQuadPlane(AutoTest):
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self.MidAirDisarmDisallowed,
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self.MidAirDisarmDisallowed,
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self.BootInAUTO,
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self.BootInAUTO,
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self.Ship,
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self.Ship,
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self.MAV_CMD_NAV_LOITER_TO_ALT,
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])
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])
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return ret
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return ret
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