The sidestep manoeuvre is investigated in some detail for a slender-wing aircraft by specifying the bank-angle time history and determining the required control angles. The effect of inclusion of the full inertia terms, ...

Summary. The rotation and flare-up phases of the take-off of a slender-wing supersonic transport aircraft are studied by calculating the time histories of speed, height, etc. when the pitch-attitude time history is specified. ...