Estimation architecture for future autonomous vehicles

Proceedings of the American Control Conference

Volumn 2, Issue , 2002, Pages 1108-1114

  Brunke, Shelby ^a   Campbell, Mark ^a  

^a UNIVERSITY OF WASHINGTON   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; CONTROL SYSTEM SYNTHESIS; KALMAN FILTERING; NONLINEAR CONTROL SYSTEMS; ROBOTICS; ROBUSTNESS (CONTROL SYSTEMS); SPURIOUS SIGNAL NOISE; STATE ESTIMATION; UNMANNED VEHICLES;

AUTONOMOUS AIRCRAFT; AUTONOMOUS VEHICLE; UNINHABITATED AERIAL VEHICLE; UNSCENTED KALMAN FILTER;

IDENTIFICATION (CONTROL SYSTEMS);

EID: 0036055690     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2002.1023167     Document Type: Conference Paper

References (25)

1. Towards intelligent autonomous control systems: Architecture and fundamental issues
2. Autonomous control reconfiguration
3. Multivariable adaptive algorithms for reconfigurable flight control
4. Autonomous failure detection, identification and fault-tolerant estimation with aerospace applications
5. System identification for adaptive and reconfigurable control
6. Parameter estimation for flight vehicles
7. Regularization techniques for real-time identification of aircraft parameters
8. Development and flight testing of a parameter identification algorithm for reconfigurable control
9. Parameter estimation of an unstable aircraft using an extended Kalman filter
10. Aerodynamic parameter estimation for higher performance aircraft using extended Kalman filtering
11. On-line aircraft state and stability derivative estimation using the modified gain extended Kalman filter
12. A new method for the nonlinear transformation of means and covariances in filters and estimators
13. Asymptotic behavior of the extended Kalman filter as a parameter estimator for linear systems
14. Development of a nonlinear simulation for the McDonnell Douglas F-15 eagle with a longitudinal TECS control law
15. Total least squares estimation of aerodynamic model parameters from flight data
16. Model predictive neural control of a high-fidelity helicopter model
17. Application of the UKF to real time estimation on the aerosonde
18. Determination of nonlinear aerodynamic coefficients using the estimation-before-modeling method
19. Nonlinear filtering and system identification algorithms for complex autonomous systems
20. On-line nonlinear guaranteed estimation with application to a high performance aircraft