I thought I answered the pressurisation question on the previous page. ALL OF THE RUMOURS ARE UTTER RUBBISH.
These systems are always operated in automatic mode. They are a PITA to operate manually, and it will only be done as a result of system failures that force their operation as part of an ECAM/EICAS or emergency checklist.
Temperature can be controlled within a restricted range, and that can be delegated to the cabin crew systems on some aircraft. Even then the range is restricted, and it would be rare to see it out of the 21-26º range, (unless the system is operating in a degraded, averaging, mode).
The 787 does operate at a bigger differential pressure than older aircraft. This results in the cabin being about 700' lower at the cruise than in previous aircraft. The A380 operates at 8.7 psi, which if memory serves correctly, is exactly the same number that the 747 used. In any event, the cabin isn't much lower. To be honest, I think this is all marketing b/s. A larger differential will also make any depressurisation more interesting.
This is what two of the pages that show pressurisation data look like at various points in the cruise.....
The above page is the synoptic that is displayed about 99% of the time in the cruise. Note that it shows that cabin vertical speed is in Auto mode (and zero fps). The cabin altitude is also in auto, with the cabin at 5,800 feet. Differential pressure is 8.6 psi. Not shown on that page, but the actual altitude was 34,000 feet.
This page is the actual pressurisation synoptic. It's from much later in the flight, and the aircraft was now up at 40,000 feet. Differential has now gone to 8.7 psi (the max), with the cabin at 6,850 feet. Again, all of the control (for cabin alt, v/s, and the packs themselves) is automatic.