Nonlinear estimation of aircraft models for on-line control customization

IEEE Aerospace Conference Proceedings

Volumn 2, Issue , 2001, Pages 2621-2628

  Campbell, M E ^a   Brunke, S ^a  

^a UNIVERSITY OF WASHINGTON   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; FLIGHT DYNAMICS; KALMAN FILTERING; NONLINEAR EQUATIONS; PARAMETER ESTIMATION;

NONLINEAR AIRCRAFT;

AIRCRAFT;

EID: 0034841191     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. System identification for adaptive and reconfigurable control
2. Multivariable adaptive algorithms for reconfigurable flight control
3. Towards intelligent autonomous control systems: Architecture and fundamental issues
4. A new approach for filtering nonlinear systems
5. Parameter estimation for flight vehicles
6. Asymptotic behavior of the extended Kalman filter as a parameter estimator for linear systems
7. On-line aircraft state and stability derivative estimation using the modified gain extended Kalman filter