Improved mass iteration schemes#143
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ian-ross
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Jun 18, 2026
| fuelBurned = self.starting_mass - traj.aircraft_mass[-1] | ||
| mass_residual = (self.total_fuel_mass - fuelBurned) / self.total_fuel_mass | ||
| delta = (fuelBurned - self.total_fuel_mass) / self.total_fuel_mass | ||
| lamda = self.total_fuel_mass / self.starting_mass |
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This PR adds the ability to use different mass iteration schemes when trying to ensure loaded vs. burned fuel in a given mission are equal. These are:
A example notebook showing differences in the three methods, as well as standalone documentation were added as well.