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making consistent with the website
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planes committed Mar 21, 2020
1 parent 42a916a commit 9ed0a56
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Showing 3 changed files with 5 additions and 5 deletions.
2 changes: 1 addition & 1 deletion Solar_UAV_Optimization/Missions.py
Original file line number Diff line number Diff line change
Expand Up @@ -57,7 +57,7 @@ def mission(analyses,vehicle):
# segment attributes
segment.state.numerics.number_control_points = 50
segment.dynamic_pressure = 115.0 * Units.pascals
segment.start_time = time.strptime("Tue, Jun 21 11:00:00 2017", "%a, %b %d %H:%M:%S %Y",)
segment.start_time = time.strptime("Tue, Jun 21 11:00:00 2020", "%a, %b %d %H:%M:%S %Y",)
segment.altitude = 1000.0 * Units.feet
segment.distance = 1000.0 * Units.km
segment.charge_ratio = 1.0
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6 changes: 3 additions & 3 deletions tut_mission_B737.py
Original file line number Diff line number Diff line change
Expand Up @@ -582,7 +582,7 @@ def configs_setup(vehicle):
config.tag = 'cutback'
config.wings['main_wing'].control_surfaces.flap.deflection = 20. * Units.deg
config.wings['main_wing'].control_surfaces.slat.deflection = 20. * Units.deg
config.max_lift_coefficient_factor = 1. #0.95
config.max_lift_coefficient_factor = 1.

configs.append(config)

Expand All @@ -595,7 +595,7 @@ def configs_setup(vehicle):

config.wings['main_wing'].control_surfaces.flap.deflection = 30. * Units.deg
config.wings['main_wing'].control_surfaces.slat.deflection = 25. * Units.deg
config.max_lift_coefficient_factor = 1. #0.95
config.max_lift_coefficient_factor = 1.

configs.append(config)

Expand All @@ -608,7 +608,7 @@ def configs_setup(vehicle):

config.wings['main_wing'].control_surfaces.flap.deflection = 20. * Units.deg
config.wings['main_wing'].control_surfaces.slat.deflection = 20. * Units.deg
config.max_lift_coefficient_factor = 1. #0.95
config.max_lift_coefficient_factor = 1.

configs.append(config)

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2 changes: 1 addition & 1 deletion tut_solar_uav.py
Original file line number Diff line number Diff line change
Expand Up @@ -412,7 +412,7 @@ def mission_setup(analyses,vehicle):

# segment attributes
segment.state.numerics.number_control_points = 64
segment.start_time = time.strptime("Tue, Jun 21 11:30:00 2017", "%a, %b %d %H:%M:%S %Y",)
segment.start_time = time.strptime("Tue, Jun 21 11:30:00 2020", "%a, %b %d %H:%M:%S %Y",)
segment.altitude = 15.0 * Units.km
segment.mach = 0.12
segment.distance = 3050.0 * Units.km
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