Use Aircraft.Design.LANDING_TO_TAKEOFF_MASS_RATIO for GASP based#1158
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xjjiang wants to merge 9 commits into
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Use Aircraft.Design.LANDING_TO_TAKEOFF_MASS_RATIO for GASP based#1158xjjiang wants to merge 9 commits into
xjjiang wants to merge 9 commits into
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…based mass subsystem.
xjjiang
changed the title
…SS_MASS for gear mass
… GASP_landing_mass
xjjiang
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Summary
Aircraft.Design.TOUCHDOWN_MASS_MAXin GASP based mass subsystem and use it to replaceAircraft.Design.GROSS_MASSin gear mass computation.landing.py.test_landing.py. In particular, we tried to avoid usingget_option_defaults().This enhancement implements GASP feature for
IWLD = 0andIWLD = 2. ForIWLD = 1, GASP uses the mission weight. We will not use this option in pre-mission analysis.Note: In GASP based subsystem,
Aircraft.Design.LANDING_TO_TAKEOFF_MASS_RATIOis a user input.Related Issues
Backwards incompatibilities
None
New Dependencies
None