发明名称 POSITIONING SYSTEM DATA INTEGRATOR USING SATELLITE AND DISTRIBUTION SYSTEM
摘要 PROBLEM TO BE SOLVED: To improve a weapon system for providing hot start navigation information for a satellite using positioning system receiver of a missile before a flight, by eliminating a part of cost and disadvantage in an advance technology. SOLUTION: This weapon control system provides the hot start navigation information for the satellite using positioning system receiver of the missile before a flight. This system has the satellite using positioning system receiver for decoding a P(Y) signal from one or a plurality of satellite using positioning system constellations of satellites, by using a classified red cipher key. When the P(Y) signal is decoded once, one or a plurality of characteristics (for example, PRN code synchronization, a Doppler shift and a modulation bit sequence) of the signals is derived. Next, the other information of a black cipher key including the characteristics and the red cipher key of these signals, is provided for the satellite using positioning system receiver of the missile before a flight. This information is provided for the missile, and the missile can acquire the P(Y) signal, and thereby, the missile can quickly determine its position more quickly than the other method. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005061820(A) 申请公布日期 2005.03.10
申请号 JP20040231009 申请日期 2004.08.06
申请人 LOCKHEED MARTIN CORP 发明人 ACAMPORA ARTHUR JR;ANDERSON DONALD B;ANTHONY RICHARD M;NGUYEN LONG T
分类号 G01S19/48;F41G7/00;F41G7/30;G01S19/09;G01S19/39;G08G5/00;H04K1/00;H04L9/08;(IPC1-7):F41G7/30;G01S5/14 主分类号 G01S19/48
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