G - Physics – 01 – S
Patent
G - Physics
01
S
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.
Alcatel Sel Aktiengesellschaft
Smart & Biggar
LandOfFree
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