DocumentCode
1862046
Title
Helicopter in-flight tracking system (HITS) test and evaluation project in the Gulf of Mexico
Author
Geyer, Michael
Author_Institution
US DOT Volpe Center, Cambridge, MA, USA
Volume
2
fYear
2001
fDate
37165
Abstract
NASA Ames Research Center is sponsoring deployment and testing of the Helicopter In-flight Tracking System (HITS) in a portion of the Gulf of Mexico offshore area. The Volpe Center is supporting NASA in managing HITS installation and operation, and in evaluating its effectiveness as an aircraft surveillance system. Sensis Corporation is supplying, installing and maintaining the HITS ground system. This project is being performed in coordination with the FAA and local helicopter operators. HITS is a dual-technology surveillance system HITS employs multilateration and automatic dependent surveillance-broadcast to obtain location and other information on helicopters and fixed wing aircraft operating near Intracoastal City, LA and in the adjacent offshore area. This paper describes the HITS project specifically, the system architecture, sensors, coverage, and test approach
Keywords
air traffic control; aircraft communication; ground support systems; helicopters; radio tracking; radionavigation; surveillance; transponders; Gulf of Mexico offshore airspace; Mode S transponders; air traffic control; aircraft surveillance system; automatic dependent surveillance-broadcast; beacon surveillance; coverage; dual-technology surveillance system; ground system; helicopter in-flight tracking system; instrumented project aircraft; low-altitude trajectories; multilateration; sensors; system architecture; target-of-opportunity aircraft; test approach; Air transportation; Aircraft; FAA; Helicopters; NASA; Radar tracking; Sensor systems; Surveillance; System testing; US Department of Transportation;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems, 2001. DASC. 20th Conference
Conference_Location
Daytona Beach, FL
Print_ISBN
0-7803-7034-1
Type
conf
DOI
10.1109/DASC.2001.964196
Filename
964196
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