| Nonlinear filtering for sequential spacecraft attitude estimation with real data: Cubature Kalman Filter, Unscented Kalman Filter and Extended Kalman Filter RV Garcia, PCPM Pardal, HK Kuga, MC Zanardi Advances in Space Research 63 (2), 1038-1050, 2019 | 122 | 2019 |
| Single frequency GPS measurements in real-time artificial satellite orbit determination APM Chiaradia, HK Kuga, AFBA Prado Acta Astronautica 53 (2), 123-133, 2003 | 46 | 2003 |
| Satélites Artificiais–Movimento Orbital HK Kuga, KR Rao, V Carrara INPE-São José dos Campos, 2011 | 39 | 2011 |
| Filtering the GPS navigation solution for real time orbit determination using different dynamical models VM Gomes, A Prado, HK Kuga Proceedings: Recent Advances in Applied and Theoretical Mechanics, 63-67, 2009 | 39 | 2009 |
| Fundamentos de tecnologia espacial A Prado, HK Kuga São José dos Campos: INPE 220, 2001 | 39 | 2001 |
| CBERS simulator mathematical models H Fuming, HK Kuga CBTT Project, CBTT/2000/MM/001, 1999 | 38 | 1999 |
| Unscented Kalman filter applied to the spacecraft attitude estimation with euler angles RV Garcia, HK Kuga, MCFPS Zanardi Mathematical Problems in Engineering 2012, 2012 | 36 | 2012 |
| Analysis of attitude determination methods using GPS carrier phase measurements L Baroni, HK Kuga Mathematical Problems in Engineering 2012, 2012 | 27 | 2012 |
| Estimating friction parameters in reaction wheels for attitude control V Carrara, HK Kuga Mathematical Problems in Engineering 2013, 2013 | 26 | 2013 |
| Introdução à mecânica orbital HK KUGA, KR Rao, V Carrara São José dos Campos: INPE, 1995 | 26 | 1995 |
| Onboard and real-time artificial satellite orbit determination using GPS APM Chiaradia, HK Kuga, AFB de Almeida Prado Mathematical Problems in Engineering 2013, 2013 | 25 | 2013 |
| Flight dynamics operations during leop for the INPE’s second environmental data collecting satellite SCD2 HK Kuga, V Orlando, RVF Lopes Journal of the Brazilian Society of Mechanical Sciences 21, 339-344, 1999 | 25 | 1999 |
| Comparison between two methods to calculate the transition matrix of orbit motion APM Chiaradia, HK Kuga, AFBA Prado Mathematical Problems in Engineering 2012, 2012 | 24 | 2012 |
| Unscented Kalman filter for spacecraft attitude estimation using quaternions and euler angles RV Garcia, HK Kuga, MC Zanardi Journal of Aerospace Engineering 3 (3), 51, 2011 | 24 | 2011 |
| A fast in-field coarse alignment and bias estimation method for stationary intermediate-grade IMUs FO Silva, EM Hemerly, WC Leite Filho, HK Kuga IEEE Transactions on Instrumentation and Measurement 67 (4), 831-838, 2018 | 22 | 2018 |
| Noções práticas de técnicas de estimação HK Kuga Class Notes of Optimization on Dynamical Systems II", INPE, São José dos …, 2005 | 22 | 2005 |
| Application of the extended H∞ filter for attitude determination and gyro calibration WR Silva, HK Kuga, MC Zanardi 24th AAS. In AAIA Space Flight Mechanics Meeting, 1-15, 2014 | 20 | 2014 |
| Robustness assessment between sigma point and extended Kalman filter for orbit determination P Pardal, HK Kuga, RV de Moraes Journal of Aerospace Engineering, Sciences and Applications 3 (3), 35-44, 2011 | 20 | 2011 |
| Algorithms for on-board orbit determination using GPS OBODE-GPS APM Chiaradia, E Gill, O Montenbruck, HK Kuga, A Prado | 20 | 2000 |
| INPES's flight dynamics team experience throughout four years of SCD-1 in-orbit operation: Main issues, improvements and trends V Orlando, RVF Lopes, HK Kuga Space Flight Dynamics, Proceedings of the 12th International Symposium held …, 1997 | 20 | 1997 |
Paula Cristiane Pinto Mesquita PardalR&D, Center of Engineering and Product Development, CEiiAVerified email at ceiia.com
