Inertial measuring units for future-generation aerospace products: fault-tolerance

Autor: L. V. Vodicheva, L. N. Bel'skiy, Yu. V. Parysheva, A. A. Lystsov

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 1, Pp 28-44 (2018)

A Strapdown Inertial Measurement Unit (SIMU) with structural redundancy intended for improving fault-tolerance and accuracy of inertial navigation systems for space applications is considered. The SIMU includes six angular rate sensors and six accele

Externí odkaz: https://doaj.org/article/5a8fcd6344a54d61a8878458ff967631