Bi-Objective Switching Control Design for a Tradeoff between Acceleration and Unstart in Hypersonic Airframe/Propulsion Models
54th AIAA Aerospace Sciences Meeting
2016-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Unstart margin control of hypersonic inlets
Online Contents | 2010
|Unstart margin control of hypersonic inlets
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|Unstart margin control of hypersonic inlets
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|Hypersonic airbreathing propulsion/airframe integration
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|Hypersonic Airbreathing Propulsion/Airframe Integration
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