PIVIT => PIVOT
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@ -266,7 +266,7 @@ JACCUV CS COEFFQ
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# THIS SECTION COMPUTES THE RATE OF CHANGE OF ACCELERATION DUE TO THE ROTATION OF THE GIMBALS. THE EQUATION
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# THIS SECTION COMPUTES THE RATE OF CHANGE OF ACCELERATION DUE TO THE ROTATION OF THE GIMBALS. THE EQUATION
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# IMPLEMENTED IN BOTH THE Y-X PLANE AND THE Z-X PLANE IS -- D(ALPHA)/DT = TL/I*D(DELTA)/DT, WHERE
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# IMPLEMENTED IN BOTH THE Y-X PLANE AND THE Z-X PLANE IS -- D(ALPHA)/DT = TL/I*D(DELTA)/DT, WHERE
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# T = ENGINE THRUST FORCE
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# T = ENGINE THRUST FORCE
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# L = PIVIT TO CG DISTANCE OF ENGINE
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# L = PIVOT TO CG DISTANCE OF ENGINE
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# I = MOMENT OF INERTIA
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# I = MOMENT OF INERTIA
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LRESC CAE ABDELV # SCALED AT 2(13) CM/SEC(2)
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LRESC CAE ABDELV # SCALED AT 2(13) CM/SEC(2)
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