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@ -101,7 +101,7 @@ TEST_CASE("time of flight example 4.2", "[orbits]")
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double r = 6378; // body radius in km
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system_2body sys = systemInit(gravBodyInit(mu, r), orbitInit(a, e)); |
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// NOTE: get ToF from periapsis to true anomaly at 154.85 degrees
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// NOTE: get ToF from true anom 230 degrees to true anom at 120 degrees
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double theta_1 = 230 * M_PI / 180; |
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double theta_2 = 120 * M_PI / 180; |
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