Abstract

The increase in sophistication of shoulder and gun launched smart weapon systems have increased the demands placed on the flight motion simulator. The high spin rate and accelerations seen during launch drastically exceed the capability of the roll axes on today’s motion simulators. Improvements are necessary to the bearing and drive system to support these requirements. This paper documents the requirements, design, and testing of a flight motion simulator produced to meet these challenges. This design can be incorporated into a new flight motion simulator, or as this paper describes, can be retrofitted into an existing flight motion simulator to improve its capability.

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