Abstract The problem on restriction of aircraft motion parameters is considered. Features of constructing the logical dynamic systems of critical parameters restriction for different channels of aircraft angular motion control are shown. The problems of synthesizing such systems are considered. The simulation results are presented.
Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
Russian Aeronautics ; 62 , 1
2019
Aufsatz (Zeitschrift)
Englisch
Lokalklassifikation TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
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