A two segment approach configuration using inertially derived flight path angle to damp the glide path and upper segment approach paths is developed in the text. System performance in both head and tail winds is evaluated. Stability analysis is also presented on root locus plots for the capture and track modes. (Author)
Glide Path Augmentation with Inertial Flight Path Angle
1974
36 pages
Report
Keine Angabe
Englisch
Aeronautics , Glide path systems , Flight paths , Augmentation , Inertial systems , Glide slope , Damping , Wind shear , Aircraft landings , Turbulence , Flight simulation , Approach , Tracking , Flight control systems , Jet transport planes , Automatic pilots , Aerodynamic stability , Perturbations , Head winds , Tail winds , C-135 aircraft , KC-135 aircraft , Glide slope capture