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Verify climb rates #520
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Settings: What I got is not very reliable i think, because hand flown and VS wobbling alot (but still wobbling around at "too much" I think).
Is there any good way to measure this in a precise manner? @Octal450 Josh, maybe do you have a simple autopilot at hand, that I can plug in and that keeps the plane level and at a desired speed (which I can provide by a table)? |
Hi, Note that it will make adjustments "softly". So if you change power or such you'll need to allow a moment for it to compensate. You have to comment out the dedicated autopilot and its dialog to access it (or manually add it) Aircraft/Generic/generic-autopilot.xml (the helper file is NOT required) Kind Regards, |
Thanks Josh, will try this! what is basicly wrong? Too much lift generated? |
It'll be fine! :) |
Indeed! |
I think I found the issue: When I tuned the engine settings (not the fdm!) I used following METAR to simulate standard atmosphere: FlightGear offers now a international standard atmosphere setting: So my simulated ISA has humidity, which influence the engine and prop power. So it will need to tune the MP-alt-volumetric-efficiency-curve inside the propulsion.xml with the correct ISA-settings to match POH-Values Good thing: the fdm itself (lift, drag etc...) won`t need any changes for this issue! |
Thanks for investigating and pointing me to the correct location for tuning, @HHS81 :) Meanwhile I (temporarily) added the generic autopilot and renamed our gui file, so F11 can access the original dialog (thanks @josh, works like a charm 🥳 ). The wing leveler from the start on helps, and levelling out at the sear at about 80 knots and then activating pitch speed control and slowly shoving in the throttle makes the plane climb and for me easy to read non-bouncing values :) This is what I got now however i have a question how to read altitude: |
ok. Found out that my weather was messed up and you need to reaply when choosing it from the launcher. |
POH 5-19 Max perfomance climb
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So the values seem off for roughly one third. What is the correct approach to correct this? I'm a bit lost here, because the table is also mapped against manifold pressure, and essentially i did just check one of the power curves |
Just tried, that messes with the fuel flow and this is then all over the place. |
Playing with a simple modifier against Modifier: POH 5-19 Max perfomance climb
So this somehow sort of worked.
With the max perforance climb you are on full throttle - are we expected to initially set the mixture and then leave t there for the climb, assuming fuel flow will decrease automatically in the proper relation? (it does this somewhat closely, however i had to relean for about 1gal/h for the altitude steps) |
So confusing - you adjust something, then something else is not working anymore (the airspeeds I tested at 14.000ft where off now) Heiko - please help :) |
@hbeni Glad you like it :) Best of luck on solve your issue. @ me if you need anything. :) Kind Regards, |
https://wiki.flightgear.org/JSBSim_Engines |
No Please have a bit patience, I'm busy. |
I'm not sure the maximum climb rates still match the POH 5-18ff.
Standard atmosphere is: 15 °C /101 3 HPa = 29,92 inHg
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