Parameter estimation for over-actuated aircraft with nonlinear aerodynamics

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 510-520

  Pachter, M ^a   Chandler, P R ^b   Nelson, E ^b   Rasmussen, S ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; FLIGHT DYNAMICS; RELIGIOUS BUILDINGS;

AIRCRAFT SIMULATION; CONTROL ALLOCATION; INDIVIDUAL CONTROL; NON-LINEAR AERODYNAMICS; RELIABLE ESTIMATES; SHORT DATA WINDOW; STABILITY DERIVATIVES; SYSTEM IDENTIFICATION ALGORITHMS;

CONTROL NONLINEARITIES;

EID: 84959167608     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4046     Document Type: Conference Paper

References (7)

1. Mendel, J. M., “Discrete Techniques of Parameter Estimation”, Marcel Dekker, New York, 1973.
2. Chandler, P. R., M. Pachter and M. Mears, “System Identification for Adaptive and Reconfig-urable Control”, Journal of Guidance, Control and Dynamics, Vol. 18, No 3, May-June 1995.
3. Smith, L., P. R. Chandler and M. Pachter, “Regularization Techniques for Real-Time Identification of Aircraft Parameters”, AIAA Guidance, Navigation and Control Conference, 1997.
4. Ward, D., J. Monaco and R. Barron, “SelfDesigning Controller: Design, Simulation and Flight Test Evaluation”, Final Tech. Report for the Air Force Office of Scientific Research, Contract F49620-94-C-0087, Barron Associates, Inc., November 1996.
5. Buffington, J., P. R. Chandler and M. Pachter, “Integration of On-Line System Identification and Optimization-Based Control Allocation”, AIAA Guidance, Navigation and Control Conference, 1998, AIAA paper No. 98-4487.
6. Buffington, J., P. R. Chandler and M. Pachter, “On-Line System Identification for Aircraft with Distributed Control Effectors”, to appear in the International Journal of Robust and Nonlinear Control, Vol. 9, 1999.
7. Pachter, M., and P. R. Chandler, “Universal Linearization Concept for Extended Kalman Filters”, IEEE Trans, of Aerospace and Electronic Systems, Vol. 29, No. 3, pp. 946-962, July 1993.