Name
Abstract | ||
|---|---|---|
This paper demonstrates the application of a recently developed anti-windup technique for systems with rate-saturated actuators, to a realistic flight control example. The paper makes two contributions: firstly a new approach to tuning the anti-windup compensator is devised, allowing a transparent trade-off between performance and the size of an estimate of the region of attraction. Secondly, the anti-windup algorithm is applied to a nonlinear simulation model of the longitudinal and lateral dynamics of an experimental aircraft. The results show the potential of anti-windup to lessen an aircraft's susceptibility to pilot-induced-oscillations. This promise has since been confirmed in flight tests |
Year | DOI | Venue |
|---|---|---|
2006 | 10.1109/CDC.2006.377217 | San Diego, CA |
Keywords | DocType | ISSN |
aerospace simulation,aircraft control,control nonlinearities,control system synthesis,oscillations,vehicle dynamics,pio avoidance,antiwindup compensator,antiwindup synthesis,experimental aircraft,flight control,lateral dynamics,longitudinal dynamics,nonlinear simulation model,pilot induced oscillations,rate-saturated actuators,simulation model | Conference | 0743-1546 |
ISBN | Citations | PageRank |
1-4244-0171-2 | 2 | 0.50 |
References | Authors | |
1 | 5 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| jorge sofrony | 1 | 2 | 0.50 |
| Matthew C. Turner | 2 | 12 | 8.75 |
| ian postlethwaite | 3 | 2 | 0.50 |
| oliver brieger | 4 | 5 | 0.94 |
| d leissling | 5 | 2 | 0.50 |