An investigation of microwave landing guidance system signal requirements for conventionally equipped civilian aircraft.

Lanman, Maurice H. III

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An investigation of microwave landing guidance system signal requirements for conventionally equipped civilian aircraft.

1971-06-01
By Lanman, Maurice H. III

File Language:

English

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Details

Creators:

Lanman, Maurice H. III
Corporate Creators:

John A. Volpe National Transportation Systems Center (U.S.)
Subject/TRT Terms:

Aircraft Azimuth Digital Simulation Landing Aids Microwave Landing Systems Turbulence Wind
Publication/ Report Number:

DOT-TSC-FAA-71-24
Resource Type:

Tech Report
Corporate Publisher:

United States. Federal Aviation Administration
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.
Format:

PDF
Collection(s):

Volpe Center
Main Document Checksum:

urn:sha256:eb25479e6c7b7612637c2328ee7335d33ea09c345e6810e0766b195236bc5176
Download URL:

https://rosap.ntl.bts.gov/view/dot/9162/dot_9162_DS1.pdf
File Type:

[PDF - 34.99 MB ]

File Language:

English

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