曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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┃  ┃   l.......                                                                                                                                                                                         ┃
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  234
5     6     7     8     9     10
t, s
Fig. 6 21   Unit-step response Oateral-directional) of the general aviation airplane:
sideslip.
Dividing throughout by A8a(s) and using Cramer's rule, we obtain
Cy&    -(bi C).pS + C).4)       s(mi.- bi C).r)
CL8a    -Cipbis + I,IS2   -(CtrbiS +I1zIS2)
Cn8o   -Cnpbis - Lzls2    -CnrbiS + IzIS2
mis - bi C,.Bs - Cip
    -Cls - bi CiBs
    ~Cnp - bi CnBS
-(bi CypS + C,.*)
-CtpllIS + IxIS2
-Cnpbi S - Ixz IS2
  s(mi - bi Cvr)
-(CLrblS + IxzIS2)
 -Cn bi S + Iz1S2
           (6.235)
Let Np.8. denote the determinant in the numerator and AJar denote the determinant
in the denominator. Expanding the determinant Ntj.8., we obtain
                        Np.8a = Ap.8.S4'+ Bp.BaS3 + Cp.8"S2 + Dp.BaS             (6.236)
r
Z
-0-5
-1-5
AIRPLANE RESPONSE AND CLOSED-LOOP CONTROL          581
_ Dutch Roll Approximation
-  Complete FiRh-Order System
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