2018
DOI: 10.1017/s0263574718001029
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Integral backstepping control for trajectory and yaw motion tracking of quadrotors

Abstract: SUMMARYThis work presents a novel trajectory tracking, hovering, and yaw motion control for quadrotors subject to unknown modeling uncertainties and disturbances. Nonlinear equations of motion are used to model the quadrotor's motion without any simplifying assumptions. An integral backstepping control is developed by defining the tracking errors, their integral, and their first through third time derivatives as the system states. The resulting surge force and roll and pitch moments are shown to asymptotically… Show more

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Cited by 31 publications
(10 citation statements)
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“…Next, consider the error dynamics along the thrust direction represented by (26) and define the Lyapunov function candidate…”
Section: Backstepping Control Law Designmentioning
confidence: 99%
“…Next, consider the error dynamics along the thrust direction represented by (26) and define the Lyapunov function candidate…”
Section: Backstepping Control Law Designmentioning
confidence: 99%
“…Then the problems need to be addressed here are stated as: 1. Use the DE proposed in formula (7) to estimate the nonlinear term F a = [F a (1), F a (2), F a (3)] T for compensation such that the attitude system robustness against disturbances from the unknown payloads can be enhanced.…”
Section: B Problem Propositiomentioning
confidence: 99%
“…Recently, quad-rotors have been widely applied in many areas [1]- [3], due to their merits of high maneuverability, free hovering, and vertical take-off/landing. To meet the task requirements, many effective approaches were developed, such as proportional-integral-derivative (PID) [4], linear quadratic regulator (LQR) [5], model reference adaptive control (MRAC) [6], feedback linearization (FL) [7], sliding model control (SMC) [8], back-stepping (BS) [9], and disturbance observer-based control (DOBC) [10]- [20].…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, the trajectory generation for the presented adaptive backstepping control is stated so that the quadrotor system has a feasible desired trajectory. The contributions of this paper are summarized as follows: (1) a backstepping-based adaptive control is proposed for quadrotor systems to track time-varying trajectories when the system parameters, mass and inertia, are unknown; nevertheless, dynamic parameters are required in [9,28] for regulation and in [8,29,30] for trajectory tracking, respectively; (2) the proposed adaptive tracking control is transferred to velocity control input by taking the uncertainties of motor coefficients in lifting force and moment torque, and geometric parameter into consideration; (3) a trajectory generation for both the scenarios of torque input and velocity input scenarios is presented based on the proposed adaptive backstepping controller; (4) simulation and experimental results are presented, and the proposed control algorithms could be extended to quadrotor systems in cable-suspended load, aerial transportation, cooperative transportation, and aerial manipulation.…”
Section: Introductionmentioning
confidence: 99%