Robust nonlinear motion control of a helicopter

Proceedings of the IEEE Conference on Decision and Control

Volumn 5, Issue , 2001, Pages 4586-4591

  Isidori, Alberto ^a   Marconi, Lorenzo ^b   Serrani, Andrea ^c  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b UNIVERSITY OF BOLOGNA   (Italy)

^c UNIVERSITÀ POLITECNICA DELLE MARCHE   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; HELICOPTERS; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; POSITION CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SYNCHRONIZATION; SYSTEM STABILITY; UNCERTAIN SYSTEMS;

ATTITUDE CONTROL; SINUSOIDAL SIGNALS; VERTICAL MOTION CONTROL;

MOTION CONTROL;

EID: 0035708988     PISSN: 01912216     EISSN: None     Source Type: Journal    
DOI: 10.1109/CDC.2001.980927     Document Type: Article

References (7)

1. Output regulation of nonlinear systems
2. Computation of the zero-error manifold for a problem of smooth vertical landing of a helicopter
3. Output tracking control design of a helicopter model based on approximate linearization
4. Autonomous vertical landing on a oscillating platform: An internal-model based approach
5. Semiglobal nonlinear output regulation with adaptive internal model
6. Landing an unmanned air vehicle: Vision based motion estimation and nonlinear control
7. A nonlinear small gain theorem for the analysis of control systems with saturations