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An Approach to Simpler Control Requirements
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
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A control system requirement is defined for an advanced direct lift engine designed for a typical Mach 2 fighter aircraft. The characteristics of the control system (performance, weight, reliability and maintainability, cost) are shown to be predominantly a function of the degree of simplicity of the control system requirements and somewhat less a result of the mechanization employed to meet those requirements.