Title :
MH60S/R helicopter multi-platform & Web-based crew trainer with FLIR
Author :
Ludwig, Jeremy ; Richards, Robert A.
Author_Institution :
Stottler Henke Assoc., Inc. (SHAI), San Mateo, CA, USA
Abstract :
The US Navy´s PMA-205, in conjunction with the training and simulation industry, has developed and deployed OMIA: a flexible, multi-platform, Web-based crew trainer for the Navy´s new MH-60S and MH-60R helicopters. OMIA is currently in use by HSC-2, HSC-3 and HSM-41 and is available to all crewmembers throughout the Navy. To maximize access to the trainer and to make deployment easier, OMIA is written in Java, and deployed both as a portable application and as a web application. A portable application does not require any special user rights to install; a web application is run over the internet from a browser. OMIA includes a simulation of the MH-60S/R Common Cockpit, including a FLIR capability that includes using an actual hardware FLIR hand-control unit when attached through USB. OMIA has been designed and implemented to be flexible to changing Navy needs, a design aspect which proved itself again in 2009 when OMIA´s FLIR was converted for use in the fixed wing EP-3E aircraft. OMIA illustrates solutions to three critical issues in developing low-cost training software for aircraft: quickly responding to the ever-changing demands, re-use of interface components across multiple aircraft, and providing training that can be accessed where and when it is needed.
Keywords :
Internet; Java; computer based training; helicopters; FLIR hand-control unit; Java; MH-60R helicopters; MH-60S helicopters; MH60S/R helicopter multiplatform; Web application; flexible multiplatform Web-based crew trainer; interface components; low-cost training software; portable application; Aerospace simulation; Computer displays; Gears; Hardware; Helicopters; Industrial training; Instruments; Java; Military aircraft; Military computing;
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
DOI :
10.1109/AERO.2010.5446775