You can not select more than 25 topics
Topics must start with a letter or number, can include dashes ('-') and can be up to 35 characters long.
58 lines
1.4 KiB
58 lines
1.4 KiB
# Test Configuration: Prograde Burn at Periapsis |
|
# Tests that periapsis distance is preserved during prograde burn |
|
|
|
[[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 = "TestSatellite" |
|
mass = 1000.0 |
|
parent_index = 1 |
|
# Start at periapsis of an elliptical orbit |
|
# a = 10,000 km, e = 0.3 |
|
# periapsis = 7,000 km, apoapsis = 13,000 km |
|
orbit = {semi_major_axis=1.0371e7, eccentricity=0.3, true_anomaly=0.0} |
|
|
|
[[spacecraft]] |
|
name = "TestSatelliteCrossing" |
|
mass = 1000.0 |
|
parent_index = 1 |
|
# Start at 90 degrees from periapsis for crossing test |
|
orbit = {semi_major_axis=1.0371e7, eccentricity=0.3, true_anomaly=1.57} |
|
|
|
[[maneuvers]] |
|
name = "periapsis_prograde_burn" |
|
spacecraft_name = "TestSatellite" |
|
trigger_type = "true_anomaly" |
|
trigger_value = 0.0 |
|
direction = "prograde" |
|
delta_v = 500.0 |
|
|
|
[[maneuvers]] |
|
name = "periapsis_prograde_burn_2" |
|
spacecraft_name = "TestSatellite" |
|
trigger_type = "true_anomaly" |
|
trigger_value = 0.0 |
|
direction = "prograde" |
|
delta_v = 500.0 |
|
|
|
[[maneuvers]] |
|
name = "periapsis_prograde_burn_crossing" |
|
spacecraft_name = "TestSatelliteCrossing" |
|
trigger_type = "true_anomaly" |
|
trigger_value = 0.0 |
|
direction = "prograde" |
|
delta_v = 500.0
|
|
|