Results are presented from the configuration performance study phase of the Helicopter Integrated Navigation System project. A configuration assessment is presented including processor selection, and a discussion of system architecture and configuration tradeoffs leading to a recommended configuration. Results of the system error analysis and the Kalman filter design are presented demonstrating integrated system performance.
Configuration Design of a Helicopter Integrated Navigation System
1987
9 pages
Report
No indication
English
The Honeywell/DND helicopter integrated navigation system (HINS)
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