[图书][B] Применение теории нелинейной фильтрации в задачах обработки навигационной информации

ОА Степанов - 2003 - elibrary.ru
Излагаются основы и специфика применения методов теории нелинейной
фильтрации марковских последовательностей и процессов в задачах обработки …

Nonlinear attitude filtering methods

FL Markley, J Crassidis, Y Cheng - AIAA guidance, navigation, and …, 2005 - arc.aiaa.org
This paper provides a survey of modern nonlinear filtering methods for attitude estimation.
Early applications relied mostly on the extended Kalman filter for attitude estimation. Since …

A drift eliminated attitude & position estimation algorithm in 3d

R Zhi - 2016 - scholarworks.uvm.edu
Inertial wearable sensors constitute a booming industry. They are self contained, low
powered and highly miniaturized. They allow for remote or self monitoring of health-related …

Satellite angular rate estimation from vector measurements

R Azor, IY Bar-Itzhack, RR Harman - Journal of Guidance, Control, and …, 1998 - arc.aiaa.org
SMALL inexpensive satellites that do not carry gyroscopes onboardstillneedtheangularratevectorforattit…
and for control loop damping. The same necessity also exists in gyro …

Неинвариантные алгоритмы обработки информации инерциальных навигационных систем

СП Дмитриев, ОА Степанов - Гироскопия и навигация, 2000 - elibrary.ru
Рассматриваются неинвариантные алгоритмы обработки информации инерциальных
навигационных систем, позволяющие учесть динамические свойства объекта …

Sequential attitude and attitude-rate estimation using integrated-rate parameters

Y Oshman, FL Markley - Journal of Guidance, Control, and Dynamics, 1999 - arc.aiaa.org
A sequential nonlinear algorithm is presented for gyroless satellite attitude and attitude-rate
estimation using vector observations. Based on a third-order, minimal-parameter method for …

Novel Kalman filtering method for the suppression of gyroscope noise effects in pointing and tracking systems

MC Algrain, DE Ehlers - Optical engineering, 1995 - spiedigitallibrary.org
A primary cause of degraded performance in pointing and tracking systems is the jitter in the
line of sight. This jitter is caused by the residual angular motion of the stabilized platform …

Suppression of gyroscope noise effects in pointing and tracking systems

MC Algrain, DE Ehlers - Acquisition, Tracking, and Pointing …, 1994 - spiedigitallibrary.org
A primary cause of degraded performance in pointing and tracking systems is the jitter in its
line-of-sight. This jitter is caused by the residual angular motion of the stabilized platform …

[PDF][PDF] Unscented Kalman filtering for spacecraft attitude and rate determination using magnetometer

SW Kim, M Abdelrahman, SY Park, KH Choi - J. Astron. Space Sci, 2009 - researchgate.net
Abstract An Unscented Kalman Filter (UKF) for estimation of the attitude and rate of a
spacecraft using only magnetometer vector measurement is developed. The attitude …

Control in computationally constrained environments

R Bhattacharya, GJ Balas - IEEE transactions on control …, 2009 - ieeexplore.ieee.org
In this paper, we present a novel algorithm for implementing linear time invariant controllers
in computationally constrained environments. The algorithm transforms a linear time …