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74 lines
1.5 KiB
74 lines
1.5 KiB
# Test Configuration: Prograde Burn at Periapsis |
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# Tests that periapsis distance is preserved during prograde burn |
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[[bodies]] |
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name = "Sun" |
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mass = 1.989e30 |
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radius = 6.96e8 |
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parent_index = -1 |
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color = { r = 1.0, g = 1.0, b = 0.0 } |
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orbit = { |
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semi_major_axis = 0.0, |
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eccentricity = 0.0, |
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true_anomaly = 0.0 |
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} |
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[[bodies]] |
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name = "Earth" |
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mass = 5.972e24 |
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radius = 6.371e6 |
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parent_index = 0 |
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color = { r = 0.0, g = 0.5, b = 1.0 } |
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orbit = { |
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semi_major_axis = 1.496e11, |
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eccentricity = 0.0, |
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true_anomaly = 0.0 |
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} |
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[[spacecraft]] |
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name = "TestSatellite" |
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mass = 1000.0 |
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parent_index = 1 |
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# Start at periapsis of an elliptical orbit |
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# a = 10,000 km, e = 0.3 |
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# periapsis = 7,000 km, apoapsis = 13,000 km |
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orbit = { |
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semi_major_axis = 1.0371e7, |
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eccentricity = 0.3, |
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true_anomaly = 0.0 |
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} |
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[[spacecraft]] |
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name = "TestSatelliteCrossing" |
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mass = 1000.0 |
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parent_index = 1 |
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# Start at 90 degrees from periapsis for crossing test |
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orbit = { |
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semi_major_axis = 1.0371e7, |
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eccentricity = 0.3, |
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true_anomaly = 1.57 # 90 degrees (pi/2) |
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} |
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[[maneuvers]] |
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name = "periapsis_prograde_burn" |
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spacecraft_name = "TestSatellite" |
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trigger_type = "true_anomaly" |
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trigger_value = 0.0 |
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direction = "prograde" |
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delta_v = 500.0 |
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[[maneuvers]] |
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name = "periapsis_prograde_burn_2" |
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spacecraft_name = "TestSatellite" |
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trigger_type = "true_anomaly" |
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trigger_value = 0.0 |
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direction = "prograde" |
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delta_v = 500.0 |
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[[maneuvers]] |
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name = "periapsis_prograde_burn_crossing" |
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spacecraft_name = "TestSatelliteCrossing" |
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trigger_type = "true_anomaly" |
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trigger_value = 0.0 |
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direction = "prograde" |
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delta_v = 500.0
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