An investigation of microwave landing guidance system signal requirements for conventionally equipped civilian aircraft.
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1971-06-01
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Abstract:The report describes efforts leading to the determination of minimum suitable scan rates for the azimuth and Elevation functions of the microwave Landing Guidance System (LGS) proposed by RTCA SC-117, based on performance requirements of two conventionally equipped civilian aircraft. Two complementary methods are used; one involving a full nonlinear digital simulation, the other involving direct covariance matrix propagation. Wind and turbulence models, aircraft models and LGS models are described in detail.
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Main Document Checksum:urn:sha-512:26784b5f2ca4c7227d935951f30b6dc4474bed2606e9ee9e18ed4bf8627db00fbf7897c383144b318ba413b32879a4502ee1ec1e9077c5811c2ba05e6b0bb454
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