IDENTIFIABILITY AND IDENTIFICATION OF THE AIRCRAFT LONGITUDINAL MOTION WITH THE MAXIMUM LIKELIHOOD METHOD
DOI:
https://doi.org/10.18372/2306-1472.24.1153Abstract
The peculiarities of the identification problem of the longitudinal motion of one aircraft class according to flight test records in the presence of intensive noises are considered. It is shown, that for the given aircraft class with the given input signals only identification of the short period component of the longitudinal motion is possible. The identification of the short period motion of aircraft using the maximum likelihood method is executed.
References
Азарсков В.М., Тунік А.А., Кліпа А.М. Розширена калманівська фільтрація в задачах оцінки стану та ідентифікації динамічних характеристик літального апарата // Електроніка та системи управління. – 2004. – № 1. – C. 114–123.
Tunik A.A., Klipa A.N. The identification of the flight dynamics models with biased sensors // Stability and Control: Theory and Applications. –2003. – Vol. 5, N 1. – P. 41–48.
Касьянов В.А., Ударцев Е.П. Определение характеристик воздушных судов методами идентификации. – М.: Машиностроение, 1988. – 170 с.
Jategaonkar R., Plaetschke E. Algorithms for Aircraft Parameter Estimation Accounting for Process and Measurement Noise // Journal of Aircraft. – 1989. – Apr. – P. 360–372.
McLean D. Automatic flight control systems. – Prentice Hall, 1990. – 593 p.
Касьянов В.А. Моделирование полета: Монография. – К.: НАУ, 2004. – 400 с.
Льюнг Л. Идентификация систем. Теория для пользователя: Пер. с англ./ Под ред. Я.З. Цыпкина. – М.: Мир, 1991. – 432 с.
Maine R., Illif K. Formulation and implementation of a practical algorithm for parameter estimation with process and measurement noise // Society of industrial and applied mathematics, Journal of applied mathematics. – 1981. – Dec. – Vol. 41, N 3. – P. 558–579.
Shanno D. Conditioning of Quasi-Newton methods for function minimization // Mathematscs of Computing. – 1970. – Vol. 24. – P. 647–656.
