In-flight identification of the augmented flight dynamics of the RMAX unmanned helicopter

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 17, Issue PART 1, 2007, Pages 217-222

  Duranti, Simone ^a   Conte, Gianpaolo ^a  

^a LINKÖPING UNIVERSITY   (Sweden)

Author keywords

Closed loop identification; Helicopter dynamics

Indexed keywords

ATTITUDE CONTROL; AUTOMATION; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; FREE FLIGHT; STABILIZATION; UNMANNED AERIAL VEHICLES (UAV);

CLOSED LOOP IDENTIFICATION; HELICOPTER DYNAMICS; SIX DEGREES OF FREEDOM; STABILITY AUGMENTATION SYSTEMS; STABILIZATION LOOP; STABILIZATION SYSTEMS; TEST INSTRUMENTATION; UNMANNED HELICOPTER;

FLIGHT CONTROL SYSTEMS;

EID: 79961001823     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20070625-5-fr-2916.00038     Document Type: Conference Paper

References (5)

1. G. Conte, S. Duranti, and T. Merz. Dynamic 3D path following for an autonomous helicopter. In Proc. of the 5th IFAC Symposium on Intelligent Autonomous Vehicles, July 2004.
2. P. Doherty. Advanced research with autonomous unmanned aerial vehicles. In Proc. of the 9th International Conference on the Principles of Knowledge Representation and Reasoning, pages 731-732, June 2004.
3. Lennart Ljung. System Identification Toolbox User's Guide For Use with Matlab. The Math-Works, 1997.
4. M. Tischler, B. Mettler, and T. Kanade. System identification modeling of a model-scale helicopter. CMU-RI-TR-00-03, 2000.
5. Yamaha Motor Co., Unmanned Helicopters. http://www.yamahamotor.co.jp/ global/industrial/sky/index.html.