Apparatus for and method of monitoring a navigation system

G - Physics – 01 – S

Patent

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343/1

G01S 1/04 (2006.01) G01S 1/02 (2006.01)

Patent

CA 2029247

Aircraft navigation systems, particularly microwave landing systems, should radiate as few erroneous sig- nals as possible and must not fail during an approach and landing operation. Both requirements have so far been met by using two monitors with equal sequences of operations and ANDing their signals. An apparatus and a method are disclosed which use monitors with dissimilar redundancy, i.e., monitors which employ the same software but have different sequences of operations.

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