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

_Ap(s)
 A8 (s~ =
                                     3.4958 x  lO-s S3 + 0.0027 S2 + 6.2143 x  10-4 S
~
            1.5586 xl0  4 S5+0 00~5 S4+0 0022S3+0 00~6 S2+6 6266 x~0 s s
           (6.258)
A~(s)
 A8a~s~ =               '.
                                     -3.4958 x  lO-s S3  - 0.0016 S2 + 0.0026 s + 0.0037
            1:5586 x  ~0 4S5 +0 00~5 S4+0 0022S3 +0 00~6 S2+6 6266 x ~0 s s
           (6.259)
A~(s)
 A8a~s~ =
                                                                   O.OOt16 S3  + 0.0046 S2 + 0.0211s
~
           1.5586 x~0 4 S5+0 00~5 S4+0.~22S3+0 00~6 S2+6 6266 x~0 s s
           (6.260)
586           PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
We note that
 Arls)       s A~(s)
A8.(s~ = A8 (s~
 Ap(s)       s A~(s)
A8a~s~ = A8 (s~
(6.261)
(6.262)
The transfer functions for the general aviation airplane for the rudder input are as
follows:
_Atj(s)
 A8r~S~ =
                      1.1093  x  10-5 S3 + 8.2661  x  10-4 S2 + 0.0064 s - 2.3475  x  10-4
          15586 x~O~ss+0~5 S4+0 0022S3+00. 0  6S2+6 6266 x~0 s s
           (6.263)
Ap(s)
A8 (s~ =
                                -7.2441  x  10-4 S3 - 0.~61S2 + 0.0015 s - 0.0018
           1.5586 x~0 4 S5 +0.~~5 S4 +0.0022 S3 +0 00  6S2+6 6266 x~0 S S
          (6.264)
A~(s)
~8~s~ =
                                           4.0151  x  10-4 S3 - 0.~~4 S2 - 0.0102 s
      1.5586 x~0- S5+0  0 5S4+0.0022S3+0  076S2+6 6266 x~0 5S
           (6.265)
Approximate /ateral-directiona/ transfer functions.
     Rollsubsidence.     Taking the Laplace transform ofEq. (6.206) for aileron input
with rudder held fixed (A8r = O) and rearranging the terms, we get
so that
A4(s)    Cl8a
Aba~s~ = s(lx S~pb )
(6.266)
   p(s)        s A~(s)
A8r(s~ = A8a~s)                     (6.267)
  Transfer functions for Dutch-roll approximation.  Taking the Laplace trans-
form of Eqs. (6.212) and (6.213) and using Cramer's rule, we obtain the following
AIRPLANE RESPONSE AND CLOSED-LOOP CONTROL          587
transfer functions for aileron defiections:
Ap(s)= Np
Aba~s~ = Alar.dr
            A~(s)= Nv,
                                                                         A8a (s)        Alat.ttr
　
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