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Upravlenie Bol'shimi Sistemami, 2017, Issue 69, Pages 76–101
(Mi ubs931)
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Remote Control and Navigation
Adaptive quaternion-based quadrotor control system
D. Nikitin Saint-Petersburg State University, Saint-Petersburg
Abstract:
In this paper we propose the quaternion-based control system for quadrotor. Adaptive scheme for thrust coefficients identification, based on speed-gradient method, is designed. Proofs of stability are provided, as well the results of numerical simulations. In existing theoretical works, Euler angles are often used as coordinates for for describing quadrotor’s coordinates. Equations using those coordinates, however, have a singularity, which prevents their use near certain points. We use quaternions instead, which have no such restrictions. The process of discovering PID-regulator coefficients is known to be tedious, error-prone and specific for each quadcopter. We propose a control scheme in which most of the parameters are physical values, and the rest do not depend on the quadcopter and can be found once for the whole class of the flying machines. An identification algorithm for obtaining physical parameters is also described. MATLAB modelling is used to test and confirm the performance of the proposed scheme.
Keywords:
UAV, quadrotor, adaptive control, speed-gradient method, quaternions.
Received: April 7, 2017 Published: September 30, 2017
Citation:
D. Nikitin, “Adaptive quaternion-based quadrotor control system”, UBS, 69 (2017), 76–101; Automation and Remote Control, 80:9 (2019), 1717–1733
Linking options:
https://www.mathnet.ru/eng/ubs931 https://www.mathnet.ru/eng/ubs/v69/p76
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Abstract page: | 754 | Full-text PDF : | 543 | References: | 64 |
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