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

U.S. Air Force T and E Days

Volumn , Issue , 2008, Pages

  Morelli, Eugene A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTICAL PROPERTIES; DETAILED DESIGN; EXPERIMENT DESIGN; FLIGHT TEST; FLIGHT TEST PROGRAMS; HYPER-X; HYPERSONIC RESEARCH VEHICLES; IN-FLIGHT DATA; INFORMATION CONTENTS; MANEUVER DESIGN; MODELING RESULTS; PRACTICAL IMPLEMENTATION; STABILITY AND CONTROL;

DESIGN; FLIGHT CONTROL SYSTEMS; HYPERSONIC AERODYNAMICS;

HYPERSONIC VEHICLES;

EID: 77958185674     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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7. nd Ed., Cambridge University Press, New York, NY, 1992, Chapter 10.
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10. Engelund, W. C., Holland, S. D., Cockrell, C., E., Bittner, R. D. "Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiment," Journal of Spacecraft and Rockets, Vol. 38, No. 6, pp. 803-810, Nov-Dec, 2001.
11. White, J.T. "HXRV First-Flight Aerodynamic Uncertainty Model," DFRC-HX-0082, November 1999.
12. Walker, S.H. and Rodgers, F. "Falcon Hypersonic Technology Overview," AIAA-2005-3253, AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, May 2005.