Does Green Dot Speed Calculation include banking Angle? I'm wondering, whether the Green Dot- speed calculation in the Airbus PFD does account for the actual bank angle of the aircraft.
Green Dot Speed is the speed for the best lift to drag ratio as it is stated in Safety first SPECIAL  EDITION: Control Your Speed Series.
In that edition, it is stated, that the Green Dot-speed is a function of aircraft weight, which is quite obvious.
I wonder however, whether the current roll angle is also accounted for as the hodographs like given in Avrenli, Kivanc, und Barry Dempsey. „Is “Green Dot” Always the Optimum Engines-Out Glide Speed on the Airbus A320 Aircraft?“ The Journal of Aviation/Aerospace Education and Research, 2015. suggests:

Any ideas how to get those numbers for Airbus aircraft?
The Green Dot speed is very stable on the PFD, unlike for example VLS which is a function of G (bank included), mach number and speed brake position.
According to Flight Crew Ops Manual(s) green dot speed varies only as a function of aircraft weight and altitude. For A320 a very crude formula is given: below 20000ft 2 x weight in tons + 85kts, above 20000ft add 1kt/1000ft.
Based on experience I would say FCOM is accurate on this matter. It wouldn't be the first time the whole truth is not revealed to the pilots, though :)