Model Formulation Over Lie Groups and Numerical Methods to Simulate the Motion of Gyrostats and Quadrotors
Keyword(s):
The present paper recalls a formulation of non-conservative system dynamics through the Lagrange–d’Alembert principle expressed through a generalized Euler–Poincaré form of the system equation on a Lie group. The paper illustrates applications of the generalized Euler–Poincaré equations on the rotation groups to a gyrostat satellite and a quadcopter drone. The numerical solution of the dynamical equations on the rotation groups is tackled via a generalized forward Euler method and an explicit Runge–Kutta integration method tailored to Lie groups.
2015 ◽
Vol 25
(11)
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pp. 2015-2042
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2008 ◽
Vol 16
(6)
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pp. 639-644
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Keyword(s):
2006 ◽
pp. 583-604
2009 ◽
Vol 47
(1)
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pp. 308-320
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2020 ◽
Vol 20
(4)
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pp. 717-725
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Keyword(s):
2015 ◽
Vol 7
(3)
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pp. 168781401557595
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