1976•NASA STI Repository (National Aeronautics and Space Administration)Open access

Control of Propulsion Systems for Supersonic Cruise Aircraft

K. W. Hiller, D. I. Drain

Abstract

The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engine, and airframe controls is discussed. The application of recent control theory developments to propulsion control design is described. Control component designs for achieving reliable, responsive propulsion control are also discussed.

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Key concepts: Propulsion, Airframe, Supersonic speed, Aeronautics, Cruise, Engineering, Component (thermodynamics), Aerospace engineering