Abstract
The standard Air Force ejection seat escape system is a vehicle which possesses unique dynamic characteristics designed for an operaticnal life saving mission within a challenging aerodynamic envelop. The combination of ejection seat equetions of motion, aerodynamic properties, and quantitative human tolerance data allows for a definition of a unique aerospace vehicle as a candidate for modern control theory design technjques. The successful application of these techniques shall yield a system design which incorporates vectored thrust digital flight control to improve ejection seat performance while operating within human tolerance limits.
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