2006
DOI: 10.1016/j.conengprac.2006.02.015
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Attitude and gyro bias estimation for a VTOL UAV

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Cited by 95 publications
(59 citation statements)
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“…Due to this fact, an additional improvement of the used navigation solution may be obtained from sensors like a navigation camera in a visual SLAM approach similar to (Georgiev and Allen, 2004). A further aspect for enhancement would be an appropriate magnetometer calibration as described in (Gebre-Egziabher, 2007, Dorveaux et al, 2009, Metni et al, 2006 or improved protection against signal interfering radiation through EMI shields. Figure 6d discloses a major problem caused by direct dependencies of navigation solution, in this case the IMU angles.…”
Section: Resultsmentioning
confidence: 99%
“…Due to this fact, an additional improvement of the used navigation solution may be obtained from sensors like a navigation camera in a visual SLAM approach similar to (Georgiev and Allen, 2004). A further aspect for enhancement would be an appropriate magnetometer calibration as described in (Gebre-Egziabher, 2007, Dorveaux et al, 2009, Metni et al, 2006 or improved protection against signal interfering radiation through EMI shields. Figure 6d discloses a major problem caused by direct dependencies of navigation solution, in this case the IMU angles.…”
Section: Resultsmentioning
confidence: 99%
“…In many cases extra sensors may facilitate the solution. For example, global positioning system (GPS) was used in [75]; magnetic field sensors were utilized in [143,68], additional bearing information was required in [11]; landmark measurements were used in [190], Earth horizon sensor was utilized in [83], active vision system was employed in [24]. Like robotic systems, living creatures solve the problem of estimation gravitational verticality using limited set of sensors.…”
Section: Verticality Estimation Methodsmentioning
confidence: 99%
“…They are in fact estimated and compensated thanks to the vision system as presented in Section 4. Under this assumption, various algorithms for attitude estimation can been considered: Kalman filter, extended Kalman filter (see Vissière [2008]) or complementary filter in both linear and nonlinear implementations (see Mahony et al [2005], Metni et al [2006], Jung and Tsiotras [2007], Mahony et al [2008], Martin and Salaün [2008]). …”
Section: Principlesmentioning
confidence: 99%
“…The analytical computations can be performed following the works on large-size helicopter rotors (Johnson [1980], Prouty [1990], Leishman [2002]), and models proposed specifically for quadrotors (Metni et al [2006], Pounds et al [2006], Romero et al [2007], Guénard [2007]), one can transpose the largesize rotors modeling techniques to small-size rotors, taking into account angular rates, which are negligible at larger scales. By contrast with Mettler [2003], , one should not neglect the forward flight speed (u, v).…”
Section: Velocity Estimation Thanks To Aerodynamics Modelmentioning
confidence: 99%