| CPC B64D 45/04 (2013.01) [H01Q 3/04 (2013.01); H01Q 25/001 (2013.01)] | 8 Claims |

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1. An aircraft landing system comprising:
a landing zone comprising:
a landing pad;
a first set of landing antennas; and
a second set of landing antennas; and
an onboard receiver comprising:
a first antenna;
a second antenna;
a motor configured to rotate an antenna assembly including the first antenna and second antenna; and
at least one processor in data communication with a memory storing processor executable code for configuring the at least one processor to:
receive a first signal via the first antenna corresponding to a first vertical lobe of a landing pad;
receiving a second signal via the second antenna corresponding to a second vertical lobe of the landing pad; and
continuously monitor a signal strength of the first signal and the second signal,
wherein:
the first set of landing antennas are configured to produce a first vertical lobe having substantially equal signal strength along a first chord defining a first centerline of the landing pad; and
the second set of landing antennas are configured to produce a second vertical lobe having substantially equal signal strength along a second chord defining a second centerline of the landing pad orthogonal to the first centerline.
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