2009
DOI: 10.2514/1.39707
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Field Programmable Gate Array-Based Attitude Stabilization

Abstract: A system for determining vehicle attitude using a field programmable gate array (FPGA) and low cost gyroscopes is presented. The method is intended to support the stabilization of a short duration, unmanned aerial vehicle. Using a microelectromechanical system (MEMS) inertial sensor for the calibration and serial interface, the algorithm sidesteps concerns related to electromagnetic interference and the impact of embedded, proprietaryfilters. An Allan variance analysis is used to characterize the sensor err… Show more

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Cited by 3 publications
(2 citation statements)
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References 11 publications
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“…By Theorem 1, the bound of 1  and 2  are achieved. So we can conclude that the velocity tracking error and the moment tracking error can converge to the prescribed performance bound.…”
Section: Stabilized Analysismentioning
confidence: 83%
See 1 more Smart Citation
“…By Theorem 1, the bound of 1  and 2  are achieved. So we can conclude that the velocity tracking error and the moment tracking error can converge to the prescribed performance bound.…”
Section: Stabilized Analysismentioning
confidence: 83%
“…Optical tracking system is widely used in robot self-balance system [1], unmanned aerial vehicle [2], airborne aiming system [3] and non-strapdown seeker servo system [4].The control object of the optical tracking system is the optical tracking platform. The main factors that affect the tracking performance are the carrier speed interference and the friction torque between the shaft systems [5] [6].Two difficulties when dealing with the improvement of the system performance.…”
Section: Introductionmentioning
confidence: 99%