Flight-test experiment design for characterizing stability and control of hypersonic vehicles

Journal of Guidance, Control, and Dynamics

Volumn 32, Issue 3, 2009, Pages 949-959

  Morelli, Eugene A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPLICATION PROGRAMS; DESIGN; FLIGHT CONTROL SYSTEMS; HYPERSONIC AERODYNAMICS;

ANALYTICAL PROPERTIES; DETAILED DESIGN; EXPERIMENT DESIGN; FLIGHT TEST PROGRAMS; HYPERSONIC RESEARCH VEHICLES; INFORMATION CONTENTS; MANEUVER DESIGN; STABILITY AND CONTROL;

HYPERSONIC VEHICLES;

EID: 67149100978     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.37092     Document Type: Article

References (10)

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9. Engelund, W. C., Holland, S. D., Cockrell, C. E., and Bittner, R. D., "Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiment," Journal of Spacecraft and Rockets, Vol. 38, No. 6, Nov.-Dec. 2001, pp. 803-810. doi: 10.2514/2.3768
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