Nonlinear tracking control of the VTOL aircraft

Proceedings of the IEEE Conference on Decision and Control

Volumn 5, Issue , 2001, Pages 4592-4597

  Setlur, P ^a   Dawson, D ^a   Fang, Y ^a   Costic, B ^a  

^a AMRL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FLIGHT DYNAMICS; LYAPUNOV METHODS; MATHEMATICAL MODELS; POSITION CONTROL; SIGNAL GENERATORS; SYSTEM STABILITY; THEOREM PROVING; TRACKING (POSITION); VTOL/STOL AIRCRAFT;

GLOBALLY UNIFORMLY ULTIMATELY BOUNDED TRACKING; ORIENTATION TRACKS; POSITION TRACKS; UNDERACTUATED SYSTEMS;

NONLINEAR CONTROL SYSTEMS;

EID: 0035705437     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Output tracking for nonlinear non-minimum phase VTOL aircraft
2. A study of flight maneuvers for the PVTOL aircraft model
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5. Robust tracking and regulation control for mobile robots
6. Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
7. Robust hovering control of a PVTOL aircraft
8. A different look at output tracking: Control of a VTOL aircraft
9. A hybrid switched mode control approach for V/STOL flight control problems
10. Switched nonlinear control of a VSTOL aircraft
11. Switching in nonminimum phase systems: Applications to VSTOL aircraft
12. Non-minimum phase output reference trajectory tracking for a PVTOL aircraft