Differential equations for librational motion of gravity-oriented rigid body

EA Kosjakov, AA Tikhonov - International Journal of Non-Linear Mechanics, 2015 - Elsevier
We consider a gravity-oriented rigid body on a circular Keplerian orbit in a central
gravitational field. The motion of the body is affected by a perturbation torque given by a …

[PDF][PDF] Application of the extended H∞ filter for attitude determination and gyro calibration

WR Silva, HK Kuga, MC Zanardi - 24th AAS. In AAIA Space Flight …, 2014 - researchgate.net
This work describes the attitude determination and the gyros drift estimation using the
Extended Hю Filter for nonlinear systems. Such filter uses the Taylor series to approximate …

[PDF][PDF] Stability analysis of the spacecraft attitude with canonical variables

MC Zanardi, WR Silva, JKS Formiga… - Proceedings of the 23th …, 2013 - issfd.org
The objective of this paper is to analyze the stability of the rotational motion of a symmetrical
spacecraft, in a circular orbit. The equilibrium points and regions of stability are established …

[PDF][PDF] The extended H∞ filter for calibration and attitude determination using real data of cbers-2 satellite

WR Silva, HK Kuga, MC Zanardi - XXIV International Symposium …, 2014 - researchgate.net
This work describes the attitude and the gyros drift estimation for real satellite CBERS-2
(China Brazil Earth Resources Satellite 2) using the Second-Order Extended H∞ Filter for …

[PDF][PDF] Filtro de partículas rao-blackwellized para estimação de atitude de satélites artificiais usando dados simulados

WR Silvaa, RV Garciab, PCPM Pardalb… - Anais do 2º …, 2019 - mtc-m21c.sid.inpe.br
Nesse trabalho, o filtro de partículas Rao-Blackwellized (FPRB) foi desenvolvido para
determinação de atitude e bias de girocópios usando dados de medida simulados para …

[PDF][PDF] REGIÕES DE ESTABILIDADE DA ATITUDE DE SATÉLITES ARTIFICIAIS SIMÉTRICOS COM O TORQUE DE GRADIENTE DE GRAVIDADE

WR Silva, MC Zanardi, RES Cabette, JK Formiga - researchgate.net
REGIÕES DE ESTABILIDADE DA ATITUDE DE SATÉLITES ARTIFICIAIS SIMÉTRICOS COM
O TORQUE DE GRADIENTE DE GRAVIDADE Page 1 XVI Colóquio Brasileiro de Dinâmica …

[PDF][PDF] Regularized particle filter with roughening for gyros bias and attitude estimation using simulated measurements

W SILVA, R GARCIA, H KUGA, M ZANARDI - issfd.org
Regularized Particle Filter with Roughening for Gyros Bias and Attitude Estimation using
Simulated Measurements Page 1 Regularized Particle Filter with Roughening for Gyros Bias …

Attitude stability analyses for small artificial satellites

WR Silva, MC Zanardi, JKS Formiga… - Journal of Physics …, 2013 - iopscience.iop.org
The objective of this paper is to analyze the stability of the rotational motion of a symmetrical
spacecraft, in a circular orbit. The equilibrium points and regions of stability are established …