Output tracking of a non-linear non-minimum phase PVTOL aircraft based on non-linear state feedback control

International Journal of Control

Volumn 75, Issue 6, 2002, Pages 466-473

  Huang, Chien Shiun ^a   Yuan, King ^a  

^a NATIONAL TAIWAN UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; LINEARIZATION; LYAPUNOV METHODS; NONLINEAR CONTROL SYSTEMS; STATE FEEDBACK; SYSTEM STABILITY;

STATE FEEDBACK CONTROLLERS;

FEEDBACK CONTROL;

EID: 0037091904     PISSN: 00207179     EISSN: None     Source Type: Journal    
DOI: 10.1080/00207170210121907     Document Type: Article

References (13)

1. Output tracking for non-minimum phase VTOL aircraft
2. A study of flight maneuvers for the PVTOL aircraft
3. Output regulation of nonlinear systems
4. Flatness and defect of nonlinear systems: Introductory theory and example
5. Nonlinear control design for slightly nonminimum phase systems: Application to V/STOL aircraft
6. Equivalence of the minimum norm and gradient projection constrained optimization techniques
7. Robust hovering control of a PVTOL aircraft
8. A different look at output tracking: Control of a VTOL aircraft
9. A decomposition based control design approach to output tracking for multivariable nonlinear non-minimum phase systems
10. Nonlinear control of non-minimum phase systems: Application to the voltage and speed regulation of power systems
11. Hover control of a PVTOL using nonlinear regulator theory
12. Regulation of nonminimum phase outputs in a PVTOL aircraft