Dynamic inversion based control concept with application to an unmanned aerial vehicle

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 2, Issue , 2004, Pages 1006-1018

  Holzapfel, F ^a,b   Sachs, G ^a,b  

^a TECHNICAL UNIVERSITY OF MUNICH   (Germany)

^b Institute of Flight Mechanics and Flight Control   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMIC INVERSION; NONLINEAR SIMULATION; PSEUDO-CONTROL HEDGING; UNMANNED AERIAL VEHICLE;

AEROSPACE VEHICLES; BANDWIDTH; COMPUTER SIMULATION; FLIGHT DYNAMICS; LINEARIZATION; MANEUVERABILITY; SIGNAL PROCESSING;

UNMANNED VEHICLES;

EID: 19644368255     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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