Flight control design for a nonlinear non-minimum phase VTOL aircraft via two-step linearization

Proceedings of the IEEE Conference on Decision and Control

Volumn 1, Issue , 2001, Pages 217-222

  Saeki, Masami ^a   Sakaue, Yoshinobu ^a  

^a HIROSHIMA UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; FLIGHT DYNAMICS; HELICOPTER ROTORS; LINEARIZATION; MATHEMATICAL MODELS;

FLIGHT CONTROL DESIGN;

VTOL/STOL AIRCRAFT;

EID: 0035707328     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Flight control design using non-linear inverse dynamics
2. Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
3. Design and construction of a small ducted fan engine for nonlinear control experiments
4. Experiments on flight control of twin-rotor helicopter model based on dynamic state feedback
5. Nonlinear controller design for inverted pendulum and exact linearization method
6. Flight control design and experiment of a twin rotor helicopter model via 2 step exact linearization
7. Output tracking for nonlinear non-minimum phase VTOL aircraft
8. A different look at output tracking: Control of a VTOL aircraft
9. Robust hovering control of a PVTOL aircraft
10. A study of flight maneuvers for the PVTOL aircraft model