2016 IEEE 11th International Symposium on Applied Computational Intelligence and Informatics (SACI) 2016
DOI: 10.1109/saci.2016.7507412
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Sensor fusion with enhanced Kalman Filter for altitude control of quadrotors

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Cited by 8 publications
(6 citation statements)
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“…In order to study the kinematic law of aircraft, two coordinate systems [44] depicted in Figure 2 The rest of this paper is organized as follows. In II, dynamic models of the quadrotor are described.…”
Section: Quadrotor Dynamic Modelsmentioning
confidence: 99%
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“…In order to study the kinematic law of aircraft, two coordinate systems [44] depicted in Figure 2 The rest of this paper is organized as follows. In II, dynamic models of the quadrotor are described.…”
Section: Quadrotor Dynamic Modelsmentioning
confidence: 99%
“…In order to study the kinematic law of aircraft, two coordinate systems [44] depicted in Figure 2 According to the conversion relationship between the Euler angle and the attitude matrix, the attitude transfer matrix R b E from the geographic coordinate system to the airframe coordinate system can be obtained:…”
Section: Quadrotor Dynamic Modelsmentioning
confidence: 99%
“…Sensor fusion techniques such as extended Kalman Filtering(KF) [39], [40] and it variants [41] had been used in robotics for an object estimation [42], a robot pose estimation, localization [43], [44] and navigation [45]. Kalman filter (KF) is normally used in real time applications to fuse dynamic sensor information [46].…”
Section: A Localizationmentioning
confidence: 99%
“…Since the time of its introduction, the Kalman filter has been the subject of extensive research and application, particularly in the area of autonomous or assisted navigation. It can be applied to compute vehicle attitude by fusion of accelerometer, gyroscopes and magnetometer data (DEIBE et al, 2020;JURMAN et al, 2007), altitude by fusion of accelerometer and barometer data (HETéNYI;GóTZY;BLáZOVICS, 2016), and position by fusion of GPS and accelerometer data (CARON et al, 2006). Also, there is the attitude filter proposed by (MAHONY; HAMEL; PFLIMLIN, 2008) which is formulated as a deterministic kinematic observer on the Special Orthogonal group SO(3) driven by an instantaneous attitude and angular velocity measurements.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Thus, in the prediction step the altitude and vertical velocity are computed in Eq. (7.70), following (HETéNYI;GóTZY;BLáZOVICS, 2016).…”
Section: Altitude and Vertical Velocity Discrete Kalman Filtermentioning
confidence: 99%