Modular configurated design of strapdown inertial units
Автор: Antonova M.V., Borodulin D.S., Volyntsev A.A., Kovaleva E.Yu., Novikov L.Z., Tereshkin A.I., Zhegalin I.I.
Рубрика: Системы навигации и управления авиационно-космической техники
Статья в выпуске: 4 т.15, 2015 года.
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Various modular configurated design approaches for development of devices and components of strapdown inertial units (SIU) - assemblies of sensitive elements (ASE), modules of service electronics, module of information exchange and control (MIEC) - are described in this paper. Basic ASE are under development, each of which contains three fiber-optical gyroscopes (FOG) and three pendulous accelerometers. Each ASE variant is based on FOG with specific accuracy levels (0.3; 0.05 or 0.01 °/hr). Two basic SIU types with different device structure are considered: three-channel and six-channel units based on one or two ASE, respectively. Design features of such monoblock and two-block units are studied; their main technical characteristics are estimated.
Strapdown inertial unit, fiber-optical gyroscope, modular configuration
Короткий адрес: https://sciup.org/147155066
IDR: 147155066 | DOI: 10.14529/ctcr150411