A method of approximate input-output linearization by dynamic state feedback is presented, with the flight control of VTOL aircraft used as an example. It is shown that the closed loop system has a graceful degradation of performance as the moment-to-force coupling is increased. It is also demonstrated that the approach proposed here leads to an asymptotically stable closed loop system with guaranteed bounds on the tracking error caused by the nonminumum phase character of the system.
On the design of nonlinear controllers for flight control systems
AIAA Guidance, Navigation and Control Conference ; 1989 ; Boston, MA, United States
1989-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
High gain flight controllers for nonlinear systems
AIAA | 1989
|Robustness Analysis of Nonlinear Flight Controllers
AIAA | 2005
|Robustness Analysis of Nonlinear Flight Controllers
Online Contents | 2005
|