Helio Koiti Kuga

发表

FLIGHT DYNAMICS OPERATIONS OF INPES SATELLITE CONTROL CENTER

Valcir Orlando, Helio Koiti Kuga, 2001 .

International Symposium on Spacecraft Ground Control and Flight Dynamics, SCD1, Sao Jose dos Campos, Brazil, Feb. 7-11, 1994

Valcir Orlando, Helio Koiti Kuga, Pawel Rozenfeld, 1994 .

Real time orbit determination using GPS navigation solution

Vivian Martins Gomes, Helio Koiti Kuga, Ana Paula Marins Chiaradia, 2007 .

Precision in the orbit determination of the TOPEX/POSEIDON satellite using GPS and recursive least squares method

Helio Koiti Kuga, Rodolpho Vilhena de Moraes, Alexandre P. Alves Da Silva, 2002 .

Refinements of the GPS Kalman Estimates for the Position and Velocity of a Vehicle during High Acceleration Transients Using IMU Measurements

Marcelo Lopes de Oliveira e Souza, Helio Koiti Kuga, Alessandro Goncalves Adinolfi, 2012 .

Orbit determination using nonlinear particle filter and GPS measurements

Paula Cristiane Pinto Mesquita Pardal, Helio Koiti Kuga, Rodolpho Vilhena de Moraes, 2014 .

Static positioning determination using GPS navigation solution

Helio Koiti Kuga, Ana Paula Marins Chiaradia, R. V. F. Lopes, 2003 .

Comparing the Extended and the Sigma Point Kalman Filters for Orbit Determination Modeling Using GPS Measurements

Paula Cristiane Pinto Mesquita Pardal, Helio Koiti Kuga, Helio Koiti Kuga, 2010 .

Kalman filtering state noise adaptive estimation

Helio Koiti Kuga, Atair Rios Neto, 1983 .

Orbit Determination and Apogee Boost Maneuver Estimation Using UD-Filtering.

O. Montenbruck, E. Gill, Helio Koiti Kuga, 1991 .

Recent highlights in astrodynamics

Amit Misra, M. C. Eckstein, Moshe Guelman, 1997 .

Stepwise modeling with friction/inertia effects separation and velocity control with dynamic compensation of a reaction wheel

Valdemir Carrara, Helio Koiti Kuga, Rafael A. M. Lopes, 2019, Comput. Appl. Math..

SCDl ORBIT DETERMINATION SYSTEM: PRE-LA UNCH PREP ARATION , LEOP PERFORMANCE AND ROUTINE OPERATIONS

Helio Koiti Kuga, Kondapalli Rama Rao, 1994 .

Sequential Estimation of Apogee Boost Maneuver Parameters.

O. Montenbruck, E. Gill, Helio Koiti Kuga, 1995 .

INPES's flight dynamics team experience throughout four years of SCD-1 in-orbit operation: Main issues, improvements and trends

Valcir Orlando, Helio Koiti Kuga, Roberto V. F. Lopes, 1997 .

UNSCENTED KALMAN FILTERS AND EXTENDED H FILTER FOR SPACECRAFT ATTITUDE ESTIMATION USING QUATERNIONS

Roberta Veloso Garcia, Maria Cecília Zanardi, Helio Koiti Kuga, 2017 .