Tomorrow Patch Question

[Chiron]

i would love someone from DEKA explain a few things

 

i seek for realistic so dont got me wrong with my questions i dont care if its a limitation or not .. i seek knowledge that is all .....

 

 

-Adjusted datalink message broadcast rate

 

what are we expecting here limitation rate or speed rate ?

 

-Adjusted FM (Cm0, fuel flow etc)

 

what also we expect here in adjusted FM ( improvement or there is a wrong values to fix and limiting some )

 

next 2 i dont know them :yes:

 

so what we expect here :

 

-Corrected ISA max rate limit

 

-Enriched transonic pitching moment

[AeriaGloria]

All I can add is,

 

By ISA max rate they probably mean max value your climb/descend indicator can show.

 

Planes usually change in pitch trim a lot while transonic, we may not feel a difference since the FCS will correct but what’s important is that the FCS resisting it is being simulated.

 

I believe Cm0 is pitching moment/longitudinal stability at zero lift

[[VFA-106] Glacier]

Speaking of the patch, what does this line mean:

 

Improved C701 and WMD7 camera track stability

[uboats]

previously, DL msg broadcast too frequently, now reduced its frequency.

[festr]

what was broken on dogfight vertical scan which was mentioned in latest patch?

[LJQCN101]

- Adjusted FM (Cm0, fuel flow etc)

 

This includes the changes of ISA (Integrated Servo Actuator) rate limit which addresses the issue of deflection rates being too quick. Not really an impact on control qualities.

 

Fuel flow changes covers FF at military power at higher speeds. Previously there's a mistake that FF at MIL doesn't change with speeds.

 

Cm0 means zero lift pitching moment coefficient. This patch basically adds more variation in pitch up/down tendencies among all speed/altitude and especially in transonic regions. Not really noticeable in a level flight since the FBW is constantly trimming for 1G (thanks to the proportional-integrator). But with rapid deceleration through transonic regions at higher Gs, there should be a tendency of pitching up and overshoot some Gs. But again, it would be soon compensated by the proportional-integrator. (Not so noticeable compared to a Su-27S who don't have an integrator)

[Chiron]

This includes the changes of ISA (Integrated Servo Actuator) rate limit which addresses the issue of deflection rates being too quick. Not really an impact on control qualities.

 

Fuel flow changes covers FF at military power at higher speeds. Previously there's a mistake that FF at MIL doesn't change with speeds.

 

Cm0 means zero lift pitching moment coefficient. This patch basically adds more variation in pitch up/down tendencies among all speed/altitude and especially in transonic regions. Not really noticeable in a level flight since the FBW is constantly trimming for 1G (thanks to the proportional-integrator). But with rapid deceleration through transonic regions at higher Gs, there should be a tendency of pitching up and overshoot some Gs. But again, it would be soon compensated by the proportional-integrator. (Not so noticeable compared to a Su-27S who don't have an integrator)

 

thanks for respond keep the excellent work and hope u apply new API for SD-10 soon

[AeriaGloria]

what was broken on dogfight vertical scan which was mentioned in latest patch?

 

Check the vertical scan and ACM threads, it couldn’t scan vertically before, and instead did like 10 normalhorizontal bars instead of a few vertical ones. The current pattern should be like a smaller rectangle within a rectangle

 

Thanks LJCQN101 for the explanation it’s really appreciated!!!

Edited July 16, 2020 by AeriaGloria