Forces and moments applied to helicopter model

X, Y, Z – axes of reference;
V – velocity vector;
F_mg – gravity;
F_FUZ – aerodynamic force of fuselage;
F_RW – aerodynamic force of right wing;
F_LW – aerodynamic force of left wing;
F_RS – aerodynamic force of right stabilizer;
F_LS – aerodynamic force of left stabilizer;
F_F – aerodynamic force of vertical stabilizer;
F1_BL1...F6_BL1 – resultant forces of blade elements;
T – resultant tractive force of rotors, T =

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