@InProceedings{SilvaGaPaKuZaBa:2022:AtEsUs,
author = "Silva, William and Garcia, Roberta and Pardal, Paula and Kuga,
H{\'e}lio Koiti and Zanardi, Maria and Baroni, Leandro",
affiliation = "{Universidade de Bras{\'{\i}}lia (UnB)} and {Universidade de
S{\~a}o Paulo (USP)} and {Universidade de S{\~a}o Paulo (USP)}
and {Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Universidade Estadual Paulista (UNESP)} and {Universidade Federal
do ABC (UFABC)}",
title = "Attitude estimation using extended h-infinity particle filter
applied to China-Brazil Earth Resource Satellilte-4",
year = "2022",
organization = "International Astronautical Congress, 73.",
publisher = "IAF",
abstract = "In this resource, a comparison is made between the Extended
H-Infinity Particle Filter (EHInfPF) and the Particle Filter (PF)
both applied to attitude estimation using simulated orbit and
attitude measurement data for CBERS-4 (China Brazil Earth
Resources Satellite 4) recently in operation. A common problem
that often occurs with the particulate filter (PF) is the sample
impoverishment. Using a small number of particles, at some point
after resampling, the particles will mostly collapse towards the
same value. Increasing the number of N particles can solve the
problem but will increase the processing time. There are other
smarter ways to deal with this sample impoverishment problem, but
herein one proposes to use an extension of the H-Infinity linear
filter for the nonlinear case of attitude estimation with
non-linearity in both the dynamics and the measurement model. The
aim is to highlight and magnify the properties of the H-Infinity
filter in terms of its favorable characteristics. In the EHInfPF
the nature (dynamics and noises) is assumed to be perverse and
actively seeks to degrade our state estimate as much as possible,
but the EHInfPF deals with it aiming ultimately at robustness
using a reduce number of particles for the state estimation. The
dynamic attitude model is described by quaternions and the
available attitude sensors using for attitude estimation are two
Digital Sun Sensors (DSS) with nonlinear functions of roll, pitch,
and yaw attitude angles; two Infrared Earth Sensor (IRES) with
direct measurements of roll and pitch angles; and a triad of
mechanical gyroscopes that provide direct incremental angles or
angular velocities. The results for attitude estimation show that
it is possible to achieve precision in determining attitudes
within the prescribed requirements using the EHInfPF, with lower
computational cost and with a smaller number of particles when
compared to the standard particle filter.",
conference-location = "Paris, France",
conference-year = "18-22 Sept. 2022",
language = "en",
targetfile = "IAC-22,C1,2,2,x67915.brief.pdf",
urlaccessdate = "11 maio 2024"
}