发明名称 Integrity monitoring system for an aircraft navigation system
摘要 An integrity monitor includes means at the ground station for periodically transmitting an integrity test signal comprising a coded first portion which identifies the signal and a coded second portion which is equivalent to a predetermined quantity. The airborne station includes a decoder which determines the type of test signal received and decodes the second portion to obtain a number which, if the system is operating properly, will compare favorably with a fixed reference. If the comparison is unfavorable, an alarm is sounded.
申请公布号 US4138678(A) 申请公布日期 1979.02.06
申请号 US19770829412 申请日期 1977.08.31
申请人 THE BENDIX CORPORATION 发明人 KIRNER, ERNEST O.
分类号 G01S1/02;G01S19/48;(IPC1-7):G01S7/40 主分类号 G01S1/02
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