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54 lines
1.1 KiB
54 lines
1.1 KiB
# Test Configuration: Maneuver Sequence |
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# Sun + Earth + LEO Satellite with scheduled burns |
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# Tests time-based and true anomaly-based maneuver triggers |
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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 = "LEO_Satellite" |
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mass = 1000.0 |
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parent_index = 1 |
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orbit = { |
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semi_major_axis = 6.771e6, |
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eccentricity = 0.0, |
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true_anomaly = 0.0 |
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} |
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# LEO orbit: 400 km altitude (Earth radius 6.371e6 m + 400e3 m) |
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[[maneuvers]] |
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name = "orbit_raise_1" |
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spacecraft_name = "LEO_Satellite" |
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trigger_type = "time" |
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trigger_value = 3600.0 |
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direction = "prograde" |
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delta_v = 500.0 |
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[[maneuvers]] |
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name = "orbit_raise_2" |
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spacecraft_name = "LEO_Satellite" |
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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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