On-line nonlinear guaranteed estimation with application to a high performance aircraft

Proceedings of the American Control Conference

Volumn 1, Issue , 2002, Pages 184-190

  Scholte, Eelco ^a   Campbell, Mark E ^a  

^a Cornell University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM SYNTHESIS; FIGHTER AIRCRAFT; KALMAN FILTERING; MATHEMATICAL MODELS; MEMBERSHIP FUNCTIONS; ONLINE SYSTEMS; PARAMETER ESTIMATION; SET THEORY; STATE ESTIMATION;

EXTENDED SET MEMBERSHIP FILTER; HIGH PERFORMANCE AIRCRAFT; NONLINEAR GUARANTEED ESTIMATION;

NONLINEAR CONTROL SYSTEMS;

EID: 0036055534     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Asymptotic behavior of the extended kalman filter as a parameter estimator for linear systems
2. Development and flight testing of a parameter identification algorithm for reconfigurable control
3. A new method for the nonlinear transformation of means and covariances in filters and estimators
4. Estimation architecture for future autonomous vehicles
5. Recursive state estimation: Unknown but bounded errors and system inputs
6. Recursive state estimation for a set-membership description of uncertainty
7. Set-membership estimation for weakly nonlinear models: An application to the adaptive control of semiconductor manufacturing processes
8. Approximate set-valued observers for nonlinear systems
9. Set inversion via interval analysis for nonlinear bounded-error estimation
10. Estimation of parameter bounds from bounded-error data: A survey
11. Estimation of model quality
12. Set-membership non-linear observers with application to vehicle localisation
13. Nonlinear state estimation using forward-backward propagation of intervals
14. Development of a nonlinear simulation for the mcdonnell douglas f-15 eagle with a longitudinal tecs control law