The paper deals with features of computer-aided design of robust inertial stabilized platforms. The most important subsystems of automated design procedure are given. Basic features of mathematical and program supports are described. Hardware structure is represented. The general structural scheme of controller design based on the robust structural synthesis is shown.
Approach to computer-aided design of UAV robust inertial platforms
01.10.2017
259455 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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