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
Link To Document :
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