Modern avionics systems are becoming increasingly sophisticated as the demands for better mission performance and higher reliability continue to escalate. Many of the missions must be carried out at ultra-low altitude under all weather and visibility conditions. The increased range, speed and accuracy of modern weapon systems, impose stringent accuracy and reliability requirements upon the aircraft navigation system. To enhance mission success in a hostile environment, the pilot amongst other things needs to operate weapon systems, target acquisition and designation systems, radar detection, night vision systems and perhaps engage in air-to-air combat. This paper describes the application of Kalman filtering technology to the design and development of a multi-sensor Generic Integrated Navigation System (GINS).
Overview of a Generic Multi-Sensor Integrated Navigation System Design
1995
21 pages
Report
No indication
English
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