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Application of the non-linear filtering method to determination an optimal control of aircraft manoeuvres

Goetzendorf-Grabowski T.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

2001

nr 11

95-98

The paper presents an application of the non-linear filtering method to determination the optimal control function of the aircraft manoeuvres. Theoretical grounds of the filtering problem and the main idea of its application for the identification problem were shown. The method, originally applied to a parametrical identification was adapted to determination a control function. A mathematical model of an aircraft flight was developed for considered case. Paper shows the results of a numerical example for a fire fighting aircraft. The calculation results concern control function determination and parametrical identification as well.