| 摘要 |
In one embodiment, a passive expendable decoy for an aircraft is provided by ejecting passive radiators from the aircraft along a transmission line trailing from the aircraft and excited by a jammer on the aircraft, such that the radiators accelerate under aerodynamic drag forces to the end of the transmission line and couple energy from the transmission line to free space. This provides angular deception to a tracking radar or homing missile since the point of radiation along the transmission line is determined by the instantaneous position of the expendable radiating element. |
