Feature/ps-update-20240524

[roger-teoh]

Closes #XX

Changes

Update Poll-Schumann aircraft performance model to version-20240524

Breaking changes

Features

• PS model: Support four aircraft types, including E75L, E75S, E290, and E295
• PS model: Integrate ps_synonym_list to increase PS model aircraft type coverage to 102
• PS model: Account for increase in fuel consumption due to engine deterioration between maintenance cycle

Fixes

Internals

• Calculate rate of climb and descent (ROCD) using hydrostatic equation to improve accuracy
• Update unit tests
• PS model: Move engine performance buffer from c_t_available to tr_max
• Settr_max buffer to +20%, as recommended by Ian Poll

Tests

• [ ] QC test passes locally (make test)
• [ ] CI tests pass

Reviewer

Select @ reviewer

[roger-teoh]

@trdean1 One thing to pay more attention during the review of this branch is the change in calculating segment_rocd in the flight class. If air_temperature is available, then the segment_rocd estimate will be more accurate with a temperature correction (More important when used in aircraft performance models, probably not required when cleaning the Spire raw ADS-B data). If it is not available, then segment_rocd can still be used too. This might affect usage in other areas.

I will make some changes in pycontrails-bada too.