Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter

Author:

Chowdhary Girish,Jategaonkar Ravindra

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

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2. Applied Optimal Control: Optimization, Estimation, and Control;Bryson,1975

3. J.H. Buckland, J.L. Musgrave, B.K. Walker, On-line implementation of nonlinear parameter estimation for the space shuttle main engine, NASA TM-106097, 1992

4. R.T.N. Chen, B.J. Eulrich, J.V. Lebacqz, Development of advanced techniques for the identification of V/STOL aircraft stability and control parameters, Cornell Aeronautical Lab., Inc., USA, Report No. BM-2820-F-1, 1971

5. G. Chowdhary, S. Lorenz, Control of a VTOL UAV using online parameter identification, AIAA-2005-6409, August 2005

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