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48 lines
1.2 KiB
48 lines
1.2 KiB
# Test Configuration: Spacecraft-to-Spacecraft Rendezvous |
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# Two spacecraft in circular, coplanar LEO orbits |
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# Chaser starts in higher orbit, performs CW-based rendezvous with target |
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# Tests the complete rendezvous workflow: CW validity, guidance calculation, execution |
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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 = -1 |
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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 = 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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# ========== TARGET SPACECRAFT ========== |
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# Circular LEO orbit at 400 km altitude |
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# This is the spacecraft being rendezvoused with |
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[[spacecraft]] |
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name = "Target_Satellite" |
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mass = 500.0 |
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parent_index = 0 |
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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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inclination = 0.0, |
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longitude_of_ascending_node = 0.0, |
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argument_of_periapsis = 0.0 |
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} |
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# ========== CHASER SPACECRAFT ========== |
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# Circular LEO orbit at 450 km altitude (slightly higher) |
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# Will perform rendezvous with Target_Satellite |
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[[spacecraft]] |
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name = "Chaser_Satellite" |
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mass = 500.0 |
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parent_index = 0 |
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orbit = { |
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semi_major_axis = 6.821e6, |
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eccentricity = 0.0, |
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true_anomaly = 0.0, |
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inclination = 0.0, |
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longitude_of_ascending_node = 0.0, |
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argument_of_periapsis = 0.0 |
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}
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