Nonlinear inversion control for a ducted fan UAV

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2005, Pages 1209-1234

  Spaulding, Christina M ^a,e   Mansu, Mohammadreza H ^b,f   Tischler, Mark B ^c,g,h   Hess, Ron A ^a,h,i   Franklin, James A ^d,h  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b UNIVERSITY OF CALIFORNIA   (United States)

^c US Army AMRDEC Development   (United States)

^d NASA AMES RESEARCH CENTER   (United States)

^e San Jose State Foundation   (United States)

^f UARC   (United States)

^g US Army Aviation and Missile Command   (United States)

^h AIAA   (United States)

ⁱ Department of Mechanical and Aeronautical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; NONLINEAR CONTROL SYSTEMS; OPTIMIZATION; ROBUSTNESS (CONTROL SYSTEMS); VELOCITY MEASUREMENT; WIND TUNNELS;

NONLINEAR INVERSION CONTROL; OUTER LOOP FEEDBACK REGULATORS; UAV; UNMANNED AERIAL VEHICLES (UAV);

UNMANNED VEHICLES;

EID: 29344459608     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6231     Document Type: Conference Paper

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