发明名称 Detection of rocket body through an active firing plume
摘要 Apparatus and a method for intercepting a rocket body during boost phase. A sensor is arranged to detect thermal emission in a range that is characteristic of a firing rocket body. The image detected by the sensor is applied to an analog-to-digital converter for digitization and application to a computer that includes a routine for separating the modulated photon energy of the detected image from the substantially unmodulated photon energy that characterizes rocket body emissions. The unmodulated photon energy, signature of the rocket body, may be utilized by a fire control system for tracking, targeting and aiming munitions at the firing rocket body.
申请公布号 US8927915(B1) 申请公布日期 2015.01.06
申请号 US201213531286 申请日期 2012.06.22
申请人 The United States of America as represented by the Secretary of the Air Force 发明人 Clark Frank O.
分类号 F41G7/22;F42B15/01;F41G7/00;F42B15/00 主分类号 F41G7/22
代理机构 代理人 Skorich James M.
主权项 1. A method for defining the image of a firing rocket body during boost phase comprising the steps of: a) selecting a detection wavelength in accordance with a boost phase temperature of said rocket body; then b) scanning a preselected region at said detection wavelength to receive a detected image characteristic of aid rocket body during boost phase; and then c) removing a component of said detected image corresponding to a plume of said firing rocket body during boost phase whereby substantially only the image of said rocket body remains.
地址 Washington DC US