Poyasakai MRF.127G Akagi-F2 .8 with FT
33.3k Bernkastel
3.4 years ago
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Auto Credit Based on Bernkastel's Poyasakai MRF.127G Akagi-F2 (Updated, Canards)
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Specifications
General Characteristics
- Predecessor Poyasakai MRF.127G Akagi-F2 (Updated, Canards)
- Created On Android
- Wingspan 43.0ft (13.1m)
- Length 62.6ft (19.1m)
- Height 17.1ft (5.2m)
- Empty Weight 22,099lbs (10,024kg)
- Loaded Weight 28,441lbs (12,901kg)
Performance
- Power/Weight Ratio 4.266
- Wing Loading 35.9lbs/ft2 (175.1kg/m2)
- Wing Area 793.2ft2 (73.7m2)
- Drag Points 3150
Parts
- Number of Parts 536
- Control Surfaces 2
- Performance Cost 3,059
@Tsukuyomi
I had to say that you are very brave that you using PID in the control system, I've been avoiding it until now that I'm making my SU-57 lol.
@GuyFolk I see, thank you
@Tsukuyomi
Tvc code can be the same code as elevator or rudder as long as the code controls same axis.
Also, you can copy code in videos so you can tune it to your liking.
Because if it is me who tuning the code it'll take a long time and I still stuck with my SU-57 flight model, been doing that for 2 weeks and I still not satisfy with it yet lol.
@GuyFolk Also for thrust vectoring, will you give her FT of it too?
@GuyFolk Will do them, thank you
@Tsukuyomi
Here are my thought.
-Try using flat-bottom wings for main wings, it'll have better stall characteristics.
-The PID code is nice and effective for controlling aoa but I think this code should be in the canards too, canards can correct aoa more precise and react faster than elevator, you can use elevator to correct aoa at low sensitivity and let the canard do the rest.
-Elevators code should be clamp(xxx,-1,1) so it'll stay in range of rotator and won't go crazy if the aoa is too much.
-If PID is too complicate you can use basic Pitch - PitchRate/xx like in my tutorial videos.
-For me I would have elevator handle pitch, pitch rate, roll, roll rate, and aoa if necessary, canards handle aoa with large range of motion and pitch rate if necessary, tvc handle pitch, pitch rate, roll, roll rate.
@GuyFolk