An Approach to Robust Control of Aircraft Motion
DOI:
https://doi.org/10.18372/1990-5548.77.18006Keywords:
aircraft control system, robust synthesis, weighting coefficients, function of mixed sensitivity, aerodynamic disturbances, lateral and longitudinal motionsAbstract
The article deals with approaches to designing aircraft control systems based on the robust synthesis. The mathematical model of the aircraft control system both for deterministic and stochastic cases is considered. The Dryden filter models are represented. The state-space conception is applied. The concept of robust designing based on H-infinity synthesis, function of the mixed sensitivity, and loop shaping is represented. The features of Robust Control Toolbox necessary for automated designing of aircraft control systems are studied. The weighting transfer functions are proposed. Results of simulation of the synthesized robust control system are shown in the form of transient processes in lateral and longitudinal motions. The proposed approach is directed on providing the possibility of the aircraft to function in conditions of influence of disturbances. The possible applications of obtained results is control of aircraft motion in civil aviation.
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