Suscripción a Biblioteca: Guest
Journal of Automation and Information Sciences

Publicado 12 números por año

ISSN Imprimir: 1064-2315

ISSN En Línea: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Satellite Correction Equations for a Strapdown Inertial System

Volumen 29, Edición 1, 1997, pp. 91-99
DOI: 10.1615/JAutomatInfScien.v29.i1.110
Get accessGet access

SINOPSIS

Equations for satellite correction of an aircraft strapdown inertial navigation system are given. Structure of equations that is suitable for estimating the error vector using a triangular Kalman filter (square-root filter) is specified. The possibility of providing the observability and obtaining estimation of the basic elements of the vector of state under the conditions of a horizontal linear flight is considered.

CITADO POR
  1. Miniature Inertial Measurement Unit, in Space Microsystems and Micro/nano Satellites, 2018. Crossref

Portal Digitalde Biblioteca Digital eLibros Revistas Referencias y Libros de Ponencias Colecciones Precios y Políticas de Suscripcione Begell House Contáctenos Language English 中文 Русский Português German French Spain