# Test Configuration: Maneuver Sequence
# Sun + Earth + LEO Satellite with scheduled burns
# Tests time-based and true anomaly-based maneuver triggers

[[bodies]]
name = "Sun"
mass = 1.989e30
radius = 6.96e8
parent_index = -1
color = { r = 1.0, g = 1.0, b = 0.0 }
orbit = {
    semi_major_axis = 0.0,
    eccentricity = 0.0,
    true_anomaly = 0.0
}

[[bodies]]
name = "Earth"
mass = 5.972e24
radius = 6.371e6
parent_index = 0
color = { r = 0.0, g = 0.5, b = 1.0 }
orbit = {
    semi_major_axis = 1.496e11,
    eccentricity = 0.0,
    true_anomaly = 0.0
}

[[spacecraft]]
name = "LEO_Satellite"
mass = 1000.0
parent_index = 1
orbit = {
    semi_major_axis = 6.771e6,
    eccentricity = 0.0,
    true_anomaly = 1.57
}
# LEO orbit: 400 km altitude (Earth radius 6.371e6 m + 400e3 m)
# Start at true_anomaly = 1.57 (90 degrees) to avoid triggering immediately

[[maneuvers]]
name = "orbit_raise_1"
spacecraft_name = "LEO_Satellite"
trigger_type = "time"
trigger_value = 3600.0
direction = "prograde"
delta_v = 500.0

[[maneuvers]]
name = "orbit_raise_2"
spacecraft_name = "LEO_Satellite"
trigger_type = "true_anomaly"
trigger_value = 0.0
direction = "prograde"
delta_v = 500.0