text: PITCH-UP., ......................................................... 
  
  Definition 
  Contribution of the airplane components 
  EFFECTS OF HIGH MACH NUMBER.. 
  
  Longitudinal stability and control 
  Directional stability 
  Dynamic stability and damping 
  
  PILOT INDUCED OSCILLATIONS.. 
  Pilot.control system-airplane coupling 
  High q aed low stick force stability 
  
  ROLL COUPLING. 
  
  Inertia and aerodynamic coupling 
  Inertia and wind axes 
  Natural pitch, yaw, and coupled pitch-yaw frequencies 
  Critical roll rates 
  Autorotative rolling 
  Operating limitations 
  
  HELICOPTER STABILITY AND CONTROL. 
  
  Rotor gyroscopic effects 
  Cyclic and collective pitch 
  Lon 
  f 
  Ang e of attack and velocity stability 
  Dynamic stability 
  
  itudinal, lateral, and directional control 
  
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