Name
Abstract | ||
|---|---|---|
This paper presents the integration of longitudinal and lateral dynamics controller designed using Nonlinear Energy Method (NEM) for a research civil aircraft. This controller ensures the core attitudes of the aircraft such as roll, pitch, yaw and airspeed follows their reference value determined by the given flight trajectory for a landing approach. The NEM is supplemented with a positional tracker on the outer loop to facilitate better positional tracking. The robustness and disturbance rejection of the proposed controller is tested in different flight conditions. Simulation result shows that the NEM is stable under scenarios such as a one-sided engine failure, a 90-degree turn, glideslopes and a wind shear. Positional tracking is also achieved in both normal and `extreme' flight conditions. |
Year | DOI | Venue |
|---|---|---|
2010 | 10.1109/CCA.2010.5611294 | Control Applications |
Keywords | Field | DocType |
aircraft landing guidance,attitude control,control system synthesis,nonlinear systems,vehicle dynamics,90-degree turn,automatic aircraft landing control,civil aircraft,disturbance rejection,flight trajectory,glideslopes,lateral dynamics controller,longitudinal dynamics controller,nonlinear energy method,one-sided engine failure,positional tracking,wind shear | Control theory,Nonlinear system,Computer science,Control theory,Attitude control,Control engineering,Robustness (computer science),Vehicle dynamics,Airspeed,Trajectory,Aerodynamics | Conference |
ISSN | ISBN | Citations |
1085-1992 | 978-1-4244-5363-4 | 1 |
PageRank | References | Authors |
0.37 | 2 | 3 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Lim Jen Nee Jones | 1 | 1 | 0.37 |
| Rini Akmeliawati | 2 | 79 | 15.22 |
| chee pin tan | 3 | 12 | 2.01 |