Abstract The problem on restriction of aircraft motion parameters is considered. The special features are noted of constructing the logical dynamic systems of automatic control with algebraic selectors for different control channels of aircraft angular motion. The problems of synthesizing such systems are considered. The simulation results are presented.
Method for constructing automatic control systems with restriction on aircraft critical parameters
Russian Aeronautics (Iz VUZ) ; 58 , 3 ; 279-285
2015-07-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Method for constructing automatic control systems with restriction on aircraft critical parameters
Online Contents | 2015
|Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
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|Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
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