Integrated approach to flight dynamics and aeroservoelasticity of whole flexible aircraft - Part II: Control design

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Meirovitcht, Leonard ^a   Tuzcu, Ilhan ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSERVOELASTICITY; AIRCRAFT CONTROL; CONTROL; ELASTIC DEFORMATION; EMPENNAGES; FLIGHT DYNAMICS; FUSELAGES; INVERSE PROBLEMS; ORDINARY DIFFERENTIAL EQUATIONS; RIGID STRUCTURES; ROTATION; STRUCTURAL DYNAMICS;

ANALYTICAL DYNAMICS; ELASTIC DISPLACEMENTS; INTEGRATED APPROACH; LINEAR QUADRATIC REGULATOR; MATHEMATICAL FORMULATION; PERTURBATION APPROACH; SPATIAL DISCRETIZATIONS; UNIFIED FORMULATIONS;

AIRCRAFT;

EID: 84896051580     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. Meirovitch, L., Dynamics and Control of Structures, John Wiley & Sons, New York, 1990.
2. Biezad, D.J., Integrated Navigation and Guidance Systems, AIAA Education Series, Reston, VA, 1999.
3. Meirovitch, L. and Tuzcu, I., "Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft," NASA Technical Report (submitted December 20, 2001).