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May 19, 2025
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Update README.md #77

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2 changes: 1 addition & 1 deletion README.md
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Expand Up @@ -33,7 +33,7 @@

- Continuous (low) thrust orbit raising/lowering between circular orbits

- Continuous (low) thrust maneuvers to change argument of perigee
- Continuous (low) thrust maneuvers to change argument of periapsis

- Note: Thrust profiles of argument of periapsis change maneuvers are calculated assuming a "continuous" maneuver takes place (i.e., a burn arc angle $\alpha = \pi/2$ radians in https://apps.dtic.mil/sti/tr/pdf/ADA384536.pdf). Therefore it is not recommended to use this feature outside of parameter ranges where this assumption does not hold. Maneuvers that take place over a fraction of an orbit are not recommended.

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