Simulation and flight control of an aeroelastic fixed wing micro aerial vehicle

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Waszak, Martin R ^a   Davidson, John B ^a   Ifju, Peter G ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT CONTROL; ANTENNAS; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; MICRO AIR VEHICLE (MAV); RIGID WINGS; STATE SPACE METHODS;

AEROELASTIC MEMBRANE WINGS; COLLABORATIVE CONTROL; FLIGHT CONDITIONS; LINEAR STATE SPACE MODEL; MEASUREMENT-BASED; MICRO AERIAL VEHICLE; NONLINEAR DYNAMIC INVERSION; SIMULATION MODEL;

FIXED WINGS;

EID: 85086612938     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4875     Document Type: Conference Paper

References (13)

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