Results of Field testing for an Integrated GPS/INS Unit based on Low-cost Redundant MEMS Sensors
暂无分享,去创建一个
Domenico Accardo | Rita Fontanella | Leopoldo Angrisani | Rosario Schiano Lo Moriello | Giorgio de Alteriis
[1] Young C. Lee,et al. A Performance Analysis of a Tightly Coupled GPS/Inertial System for Two Integrity Monitoring Methods , 1999 .
[2] George T. Schmidt,et al. Navigation sensors and systems in GNSS degraded and denied environments , 2015 .
[3] Alexandra Wander,et al. Innovative fault detection, isolation and recovery on-board spacecraft: Study and implementation using cognitive automation , 2013, 2013 Conference on Control and Fault-Tolerant Systems (SysTol).
[4] Xiaoji Niu,et al. An Accurate Land-Vehicle MEMS IMU/GPS Navigation System Using 3D Auxiliary Velocity Updates , 2007 .
[5] N. Al-Holou,et al. Accurate INS position solution during GPS outages or degraded GPS , 2005 .
[6] Daidai Chen,et al. A Novel Optimal Configuration form Redundant MEMS Inertial Sensors Based on the Orthogonal Rotation Method , 2014, Sensors.
[7] John L. Crassidis,et al. Three-Axis Attitude Estimation Using Rate-Integrating Gyroscopes , 2016 .
[8] Shaojun Feng,et al. Integrity of an integrated GPS/INS system in the presence of slowly growing errors. Part I: A critical review , 2007 .
[9] G. Rufino,et al. A procedure for three-dimensional angular velocity determination using a star sensor in high-rate rotation modes , 2001 .
[10] Shourong Wang,et al. Temperature Effects and Compensation-Control Methods , 2009, Sensors.
[11] Domenico Accardo,et al. MEMS gyros temperature calibration through artificial neural networks , 2018, Sensors and Actuators A: Physical.
[12] Tong Heng Lee,et al. Coordinate Systems and Transformations , 2011 .
[13] Mehdi Jafari,et al. Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system , 2015 .
[14] Marcello R. Napolitano,et al. Fusion of GPS and Redundant IMU Data for Attitude Estimation , 2012 .