G - Physics – 01 – S
Patent
G - Physics
01
S
343/76
G01S 1/16 (2006.01) G01S 1/10 (2006.01) G01S 1/18 (2006.01) G01S 1/56 (2006.01)
Patent
CA 1284203
ABSTRACT The invention provides independent guidance and monitoring integrated into an MLS landing system and a scaled-down MLS take-off or missed approach guidance system useable at small airports. An added fixed beam precision guidance system is integrated into the MLS time sequence format. The fixed beam guidance system is based upon the concept of using paired fixed overlapping beams, sequentially radiated by different fixed antennas (80 and 81), oriented to left and right of a prescribed guidance path. The paired beams overlap at the prescribed guidance path in such a manner that an aircraft departing or making a missed approach on such path will intercept equal signal intensities to indicate an on-course condition. Conversely, when the aircraft is off-course to one side of the prescribed path, it will intercept a stronger signal intensity for the fixed guidance beam which is directed to that side of the prescribed path and a weaker signal intensity for the fixed beam which is directed to the other side of the prescribed path.
548879
Chisholm John P.
Riches Mckenzie & Herbert Llp
Sundstrand Data Control Inc.
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