Rocket nozzle flow control using a reduced-order computational fluid dynamics model

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 3, 2002, Pages 449-454

  Lucia, David J ^a   Pachter, Meir ^a   Beran, Philip S ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLOW CONTROL; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; NOZZLES; OPTIMAL CONTROL SYSTEMS; ROCKET ENGINES;

MULTIDISCIPLINARY OPTIMIZATION; PROPER ORTHOGONAL DECOMPOSITION; ROCKET NOZZLE FLOW CONTROL;

CONTROL SYSTEM SYNTHESIS;

EID: 0036564226     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4930     Document Type: Article

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