Aircraft with weapons shaft - arrangement and method for the setting down a shaft in a weapons the weapon from the aircraft

摘要

Aircraft (1), comprising a fuselage (2) with a on an underside (2a) running gear (5) and arranged with one of these, which is arranged opposite hull-top (2b).– on the hull-top (2b) a weapon carrier - device (10) is arranged,– the weapon carrier - device (10) in the cross-section of the hull at the point of a main landing gear (5b) is considered above suspension shafts (15) of the main landing gear (5b) and above a engine - flow channel (17) is arranged,– the aircraft (1) a flight computer - device with a control method according to the - and missions - function as well as a traveling - device for the movement of the control surfaces for the control of the aircraft (1), wherein the control - and missions - function of a flight-guidance - function for the supply of the flying device (1) to a destination or drop-off point and a weapons sedimentation - function for depositing at least one in the weapon carrier - device (10) has on the basis of a specification of a portable weapon,– the aircraft (1), is in each case a of the control method according to the - and missions - function associated function and a attitudes - sensor system, with which the aircraft (1) about its longitudinal axis x_f can be rotated to such an extent, so that a component of the resulting buoyant force from the underside of the hull (2a) of counter to the force of gravity - direction, and– the flight computer - device is a heights - sensor is assigned and the control - and missions - function of a terrain a result of flight - function on the basis of the heights - sensor has determined height data.