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POWER SPECTRA FOR UNCORRELATED VERTICAL AND HORIZONTAL
SELECTED ROOT MEAN SQUARE RESPONSES FOR IDEALIZED AIRCRAFT
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aerodynamic aircraft response altitude hold altitude response angle of attack Appendix atmospheric density atmospheric turbulence attack responses buffet boundary computational constraint boundaries constraint envelope control system Covariance ellipse defined drag coefficient effects Equation Equivalent Airspeed exceedance probability feedback gain Figure 9 flight envelope frequency function gust velocity horizontal Idealized Aircraft knots lbs/ft2 lift coefficient load factor limit load factor response longitudinal Loose pitch control MACH NUMBER mass parameter mean aerodynamic chord negative load factor nondimensional nonlinear NUMBER AND ALTITUDE performance concept phugoid pitch angle pitch attitude Pitch autopilot positive load factor power spectra procedure rad/ft radians ratio responses to turbulence RESPONSES TO UNIT RMS RESPONSES rms turbulence ROOT MEAN SQUARE shown in Figure speed of sound static margin trim flight condition true airspeed turbulence model turbulence penetration turbulence-penetration performance unit turbulence inputs UNIT TURBULENCE INTENSITY values variables VARIATION vertical gust wing area wing loading