动力机械和机身手册3(76)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

                                 A8a~s~ = A8S2 + B8s
                                     Al( (s)          Ai,
                              -             (6.274)
                                   A a~s~ = A8S2 + B8s .
                                                                                                                                                                                     i
where
                                  AB = Cl8alzl                          (6.275)
                                Bp = -b] (CM,Cnr + Cn8a Clr)                      (6.276)
                                                           A8 = Ctp Izi                                           (6.277)
                                                  Bb = bi (Cnp Clr - Ctp Cn  )                                  (6.278)
                                               Aj, = CIIJ:Cn8r  + Cnp Cl8a                                 (6.279)
   Substituting the mass and aerodynamic characteristics of the general aviation
airplane, we get the approximate transfer functions of the general aviation airplane
for aileron and rudder inputs as follows.
    For the roll subsidence mode,
A~(s)      0.1342
A8a~s~ = s~0~46s+0038. .   7)
Aq3(s)     0.0118
A8~s~ = s~0 0046s+0.0387)
(6.280)
(6.281)
'1
588 PERFORMANCE,STABILITY,DYNAMICS,ANDCONTROL
     For the Dutch-roll approximation,
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：动力机械和机身手册3(76)