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Mig-21-Flight Model - Check six

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<strong>Mig</strong>-<strong>21</strong>-FM-Identification-Rev. 14<br />

If we assume that incidence angle is so small that we can also consider Thrust being along horizontal<br />

(sin(AoA) = 1.0), formula become:<br />

There is also a relation between acceleration and Extra Specific Power (or instantaneous climb rate)<br />

(V true air speed in m/s, Ps and Vz in m/s, g = 9.81 m/s 2 ), or<br />

that give the global equation system<br />

(3.3)<br />

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