Mikoyan-Gurevich MiG-29 Fulcrum - History, Design, Performance & Dissection

İs this footage from dev server or live server?

It also now has correct visual model with L-150 antennas.

Dev server

Well then time to be patient until patch drops.

Because that one is inline:
$\int^1_0 e^x dx = e$ gets you \int^1_0 e^x dx = e.,
but

$$
\int^1_0 e^x dx = e
$$

gets you

\int^1_0 e^x dx = e

Unlike regular LaTeX, if you want to use $$ x^e $$ you have to have the $$ on separate lines.

Alternatively, if you want inline math but with full-sized symbols, you can use \displaystyle like in
$\displaystyle {\int e\ dx}$ to get \displaystyle {\int e\ dx}.

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Thanks, I thought it was just regular Latex

anyone notice how much more lift the mig29 has. It seems to climb in level flight and I musdt point the nose down periodically. pretty cleaner turner the G is

it there any drag/weight penalties that come in when equipping the UV-5-08 countermeasure blocks? Not modelled? They are chunky

Yes, that’s how it should be, you have to point your nose down to keep the horizon.It will be the same on the Su-27

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what does drag/weight mean?

Yes, it’s called positive speed stability. Also in Mig-29, thrust is applied below CoG causing very pronounced pitch-up effect especially at low IAS and low altitudes. (Description from https://www.digitalcombatsimulator.com/upload/iblock/dcc/DCS%20FM%20principles%20plus%20MiG-29%20P-47%20F-16.pdf)

Mig29 trim

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Strangely, the curve actually shows negative speed stability below 0.85 mach. Positive stabilizer angle means trailing edge down, or stick forward. Here’s the one for Su-27:

su27 trim

The Su-27 is a statically unstable stable aircraft.He is constantly being pulled up.Up to supersonic speeds

Yes, statically unstable but speed stable (pitching up with increasing speed) as shown in the graph.

Su-27 has a trim schedule in the control law of pitch FBW (SDU-10) to further provide speed stability with increasing speed:
su27 pitch fbw

this is not a graphic block diagram
almost all the signatures here are not correct

It actually has all the transfer functions and gain schedules you need to replicate the control response in Matlab simulink, or code in C++.

What’s incorrect then, it’s from the SDU-10 manual.

Trim shedule,lag filter

without knowing the equations, these are all useless graphs