2020
DOI: 10.1109/lra.2020.3010214
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Finite-Horizon LQR Control of Quadrotors on $SE_2(3)$

Abstract: This paper considers optimal control of a quadrotor unmanned aerial vehicles (UAV) using the discrete-time, finite-horizon, linear quadratic regulator (LQR). The state of a quadrotor UAV is represented as an element of the matrix Lie group of double direct isometries, SE2(3). The nonlinear system is linearized using a left-invariant error about a reference trajectory, leading to an optimal gain sequence that can be calculated offline. The reference trajectory is calculated using the differentially flat propert… Show more

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Cited by 49 publications
(27 citation statements)
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References 24 publications
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“…The trajectory-tracking controller implemented is based on the finite-horizon LQR controller presented in [24]. The trajectory to be tracked is the teach pass estimated pose trajectory πt , represented at any time-step k as an element of a matrix Lie group Xt…”
Section: Lqr Controllermentioning
confidence: 99%
See 1 more Smart Citation
“…The trajectory-tracking controller implemented is based on the finite-horizon LQR controller presented in [24]. The trajectory to be tracked is the teach pass estimated pose trajectory πt , represented at any time-step k as an element of a matrix Lie group Xt…”
Section: Lqr Controllermentioning
confidence: 99%
“…and the command inputs are computed similarly to [24]. Even though the estimated teach trajectory drifts from the true trajectory, the anchors are localized based on the drifted trajectory.…”
Section: Lqr Controllermentioning
confidence: 99%
“…The LQR is a highly effective method to design an optimal full-state-feedback controller for linear, or linearized systems [78]. The correction and design of the LQR needs to find the appropriate state variables and control quantity weighting matrix according to the response curve, without determining the closed-loop pole position according to the required performance [79].…”
Section: Optimal Control (1)mentioning
confidence: 99%
“…There are several control techniques for the attitude and altitude of the quadcopter such as proportional-integralderivative (PID) control [1,2], adaptive control [3][4][5], neural network [6,7], LQR control [8,9], model predictive control [10,11], have been investigated in many studies. Comparison with other approaches, sliding mode control (SMC) [12,13] is exploited as a special and robust control algorithm against parametric uncertainties, external disturbances through its sliding surface.…”
Section: Introductionmentioning
confidence: 99%