Title :
Demonstration of the JEDI system on Joint STARS
Author :
Kish, Brian A. ; Gutierrez, Jose R. ; Evans, John A. ; Hidalgo, Ran ; Meador, C. Lawrence
Author_Institution :
Joint STARS Test Force, Melbourne, FL, USA
Abstract :
This paper presents the results of the Joint Expeditionary Digital Information (JEDI) system demonstration on the Joint Surveillance Target Attack Radar System (Joint STARS). Developed by Booz·Allen & Hamilton, the JEDI system with Iridium represents an off-the-shelf system that uses Windows CE based software that is capable of developing, exchanging, and displaying standard US Army call-for-fire messages. Together with Joint STARS, JEDI can shorten the time-critical targeting kill chain response. The demonstration involved one day of ground tests followed by one flight test mission with the Joint STARS test aircraft. All test objectives were met. The JEDI system-provides an effective way of transmitting small files (formatted text messages) through a commercial satellite network with its full duplex, 2400-baud rate capability in a non-secured mode. The Requirements Review Board for Joint STARS will evaluate JEDI and let it compete with other requirements for funding.
Keywords :
airborne radar; aircraft communication; command and control systems; data communication; digital communication; military communication; military radar; mobile satellite communication; search radar; Iridium; JEDI system; Joint Expeditionary Digital Information system; Joint STARS; Joint Surveillance Target Attack Radar System; US Army call-for-fire messages; Windows CE based software; commercial satellite network; flight test mission; formatted text message transmission; full duplex capability; nonsecured mode; off-the-shelf system; test aircraft; time-critical targeting kill chain response; Aircraft; Communication system control; Control systems; Force control; Radar tracking; Spaceborne radar; Surveillance; Synthetic aperture radar; Testing; Time factors;
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
DOI :
10.1109/AERO.2002.1035434