公开(公告)号：US5755400A

公开(公告)日：1998-05-26

申请号：US194328

申请日：1980-10-02

申请人： William Kalms, III

发明人： William Kalms, III

IPC分类号： F41G7/34

CPC分类号： F41G7/343

摘要： A technique for deriving correction signals for inertial instruments on a missile, such as an intercontinental ballistic or a cruise missile, is shown to include: a radar operative in a synthetic aperture mode when the missile approaches a predetermined area containing at least three separate fixed terrain features whose radar signatures (as observed from a preselected position) have been predetermined and stored on the missile; successively illuminating each one of such features and comparing the actual radar signals with the stored radar signatures; and deriving correction signals for the inertial instruments in accordance with the difference between the actual and stored radar signals.

摘要翻译： 用于导出导弹（如洲际弹道导弹或巡航导弹）上的惯性仪器的校正信号的技术被证明包括：当导弹接近包含至少三个独立固定地形的预定区域时，以合成孔径模式工作的雷达 其雷达签名（从预选位置观察）已被预先确定并存储在导弹上; 连续地对这些特征中的每一个进行照明，并将实际的雷达信号与存储的雷达签名进行比较; 并根据实际和存储的雷达信号之间的差异导出惯性仪器的校正信号。