Flight Test Route Structure Statistics of Helicopter GPS Navigation with the Magnavox Z-Set
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1982-12-01
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Edition:Data Report
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Abstract:The Federal Aviation Administration (FAA) Technical Center conducted this test project under Technical Program Document (TPO) 04-150 to determine the operational suitability of the Navigation Satellite Timing and Ranging Global Positioning System (NAVSTAR GPS) for rotary wing aircraft. The flight tests were conducted in a CH-53A helicopter using a prototype low-cost GPS receiver, the Magnavox Z-set. Over 15 hours of radar tracked en route and non-precision approach flight tests were flown with two-dimensional GPS derived guidance (cross-track and distance-to-go) used as the primary navigation system.
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Main Document Checksum:urn:sha-512:cdd51891d3d183133718940170c4005a52c7716cf609c30920c474c5abb8704e0966f6fe591ca6d5043264691aed6f84f58e1ee5b574dc2a29aada4d9e860309
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