FA-69809 / Orbital propagation / Member archive
Co-orbital phasing manoeuvre: Only the entry burn is budgeted · case 04
The delta-v budget omits the burn that recircularizes.
Case contract
Input [r, theta, k, mu, rmin]: circular radius, target lead angle in degrees (positive = target ahead), k phasing revolutions. Phasing period Tph=T-theta_rad/(k n). a_ph from Tph; total dv = 2|v_ph(r)-v_circ| with vis-viva at r. Return None if the phasing perigee 2a_ph-r is below rmin, else [a_ph rounded 3, dv rounded 6, k*Tph rounded 3].
Why this case matters
Orbit determination and mission planning chain many small conversions; one wrong branch or unit silently moves a spacecraft by kilometres.
One recorded failure
Sample boundary fixtureThis sample comes from the broken implementation of a controlled reproducer.
| Boundary fixture | Actual | Expected | Outcome |
|---|---|---|---|
| co-orbital phasing manoeuvre [42164.0, -45.0, 4, 398600.4418, 6478.0] | [43037.904, 0.031059, 355424.729] | [43037.904, 0.062119, 355424.729] | Failed |
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