Aeroelastic vehicle sensor placement for feedback control applications using gain stability

ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)

Volumn 2000-N, Issue , 2000, Pages 221-228

  Al Shehabi, Abdul G ^a   Newman, Brett ^a  

^a Old Dominion University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT MANUFACTURE; AIRFRAMES; OPTIMIZATION; STEEPEST DESCENT METHOD;

CONTROL REQUIREMENTS; DESIGN CONSTRAINTS; DESIGN CONTROL; FEED-BACK SENSORS; FEEDBACK CONTROL APPLICATIONS; GAIN STABILITY; OPTIMAL APPROACHES; OPTIMAL POSITION; SENSOR PLACEMENT; VEHICLE SENSORS;

STABILITY CRITERIA;

EID: 84894439221     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2000-2305     Document Type: Conference Paper

References (11)

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8. McLean, D., 1990, Automatic Flight Control Systems, Prentice Hall, Cambridge, England.
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