A collection of technical papers: AIAA Atmospheric Flight Mechanics Conference, August 11-13, 1997, New Orleans, LA.
American Institute of Aeronautics and Astronautics, 1997 - Transportation - 830 pages
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Paper No Title and Author Page
Session 8AFM2 Flight Mechanics I
14 other sections not shown
aerodynamic aerodynamic model AIAA AIAA Paper aircraft airplane algorithm altitude amplitude analysis angle of attack applied approximately bandwidth bank angle bifurcation calculated characteristics computed configuration constraint control law control surface damping deflection delay delta wing drag drag coefficient Dutch roll eigenvalues equations equilibrium error estimated evaluation feedback Figure fins flight conditions flight dynamics flight mechanics flight path flight test flow force frequency ground effect handling qualities increase initial input Journal lift coefficient limit cycle linear load longitudinal Mach number maneuver matrix method microburst missile motion NASA nonlinear obtained optimal OREX oscillations output parameters performance phase pilot model pilot-induced oscillations pitch attitude predicted pressure problem range rate limiting Research response roll angle roll rate rotor shown in Fig shows sideslip simulation solution speed stability derivatives static supersonic trajectory turbulence unsteady variables vector vehicle velocity vertical wind tunnel windshear wing rock zero