Landing areas and multi-channel trajectory control of experimental suborbital aircraft

Бесплатный доступ

Maneuverability of suborbital aircraft motion in atmosphere is discussed. Landing areas for two-channel and three-channel control are determined, with regard to constraints on control, motion modes and terminal conditions. Control programmes for the channels of the angle of attack, angle of roll and engine trust are given, which bring a suborbital aircraft to specific points of landing areas.

Короткий адрес: https://sciup.org/148197668

IDR: 148197668

Статья научная