Abstract:This paper proposes a sliding mode active disturbance rejection control scheme to deal with trajectory tracking control problems for the quadrotor unmanned aerial vehicle (UAV). Firstly, the differential signal of the reference trajectory can be obtained directly by using the tracking differentiator (TD), then the design processes of the controller can be simplified. Secondly, the estimated values of the UAV's velocities, angular velocities, total disturbance can be acquired by using extended state observer (E… Show more
“…The superiority of the proposed control structure was clearly demonstrated when compared to the conventional PID. Further, Zhang et al [174] displayed a sliding mode ADRC scheme to improve tracking control of a quadcopter system with an efficient disturbance rejection capability. The proposed control strategy performed excellently in comparison to the classical ADRC.…”
This paper presents a review of the various control strategies that have been conducted to address and resolve several challenges for a particular category of unmanned aerial vehicles (UAVs), the emphasis of which is on the rotorcraft or rotary-wing systems. Initially, a brief overview of the important relevant definitions, configurations, components, advantages/disadvantages, and applications of the UAVs is first introduced in general, encompassing a wide spectrum of the flying machines. Subsequently, the focus is more on the two most common and versatile rotorcraft UAVs, namely, the twin-rotor and quadrotor systems. Starting with a brief background on the dual-rotor helicopter and a quadcopter, the full detailed mathematical dynamic model of each system is derived based on the Euler-Lagrange and Newton-Euler methods, considering a number of assumptions and considerations. Then, a state-of-the-art review of the diverse control strategies for controlling the rotorcraft systems with conceivable solutions when the systems are subjected to the different impediments is demonstrated. To counter some of these limitations and adverse operating/loading conditions in the UAVs, several innovative control techniques are particularly highlighted, and their performance are duly analyzed, discussed, and compared. The applied control techniques are deemed to produce a useful contribution to their successful implementation in the wake of varied constraints and demanding environments that result in a degree of robustness and efficacy. Some of the off-the-shelf developments in the rotorcraft systems for research and commercial applications are also presented.
“…The superiority of the proposed control structure was clearly demonstrated when compared to the conventional PID. Further, Zhang et al [174] displayed a sliding mode ADRC scheme to improve tracking control of a quadcopter system with an efficient disturbance rejection capability. The proposed control strategy performed excellently in comparison to the classical ADRC.…”
This paper presents a review of the various control strategies that have been conducted to address and resolve several challenges for a particular category of unmanned aerial vehicles (UAVs), the emphasis of which is on the rotorcraft or rotary-wing systems. Initially, a brief overview of the important relevant definitions, configurations, components, advantages/disadvantages, and applications of the UAVs is first introduced in general, encompassing a wide spectrum of the flying machines. Subsequently, the focus is more on the two most common and versatile rotorcraft UAVs, namely, the twin-rotor and quadrotor systems. Starting with a brief background on the dual-rotor helicopter and a quadcopter, the full detailed mathematical dynamic model of each system is derived based on the Euler-Lagrange and Newton-Euler methods, considering a number of assumptions and considerations. Then, a state-of-the-art review of the diverse control strategies for controlling the rotorcraft systems with conceivable solutions when the systems are subjected to the different impediments is demonstrated. To counter some of these limitations and adverse operating/loading conditions in the UAVs, several innovative control techniques are particularly highlighted, and their performance are duly analyzed, discussed, and compared. The applied control techniques are deemed to produce a useful contribution to their successful implementation in the wake of varied constraints and demanding environments that result in a degree of robustness and efficacy. Some of the off-the-shelf developments in the rotorcraft systems for research and commercial applications are also presented.
“…In general, it is difficult to control the aircraft under highfrequency random disturbances and multi-frequency random disturbances. Here, to solve this problem, two forms of wind gusts were presented in the simulation: high frequency random disturbances (high frequency sine signal) [17,27,[35][36] and multi frequency random disturbances (square wave signal) [34,37]. The disturbances used in this tracking simulation consist of the following two parts:…”
Section: Example 2 Trajectory Tracking Simulationmentioning
confidence: 99%
“…This is especially true for hybrid controllers combined with fuzzy control algorithm. By introducing human experience into the controlling process, these intelligent algorithms guarantee an accurate approximation to the model's uncertainties [30][31][32][33][34]. When combined with an adaptive strategy, the intelligent control system allowed for real-time regulation of system parameters according to its actual state [35][36][37].…”
Section: Introductionmentioning
confidence: 99%
“… [34]. { = 1.5 (0.5 ) = 1.5 (0.5 ) = = The simulation time is 20s, initial position coordinates and attitude of the quadrotor were set as [ , , ] = [0 0 0] , [ , , ] = [0 0 0].…”
In this paper, an online adaptive control strategy is proposed for the accurate trajectory tracking of quadrotor unmanned aerial vehicles (UAVs) under time-varying model uncertainties and external disturbances. A robust sliding mode controller was developed for the outer-loop position subsystem to guarantee robust tracking performance even under disturbance. For the inner-loop attitude subsystem, an online adaptive controller was designed, which integrated the fuzzy and SMC into one unified system. Critically, its parameters were simultaneously identified and adjusted in real-time. These sub-control systems were then integrated into a unified closed-loop system. Its uniform stability was then analyzed and strictly proofed. Case studies demonstrated the effectiveness of our proposed strategy, along with its superior control performance when compared with several commonly used methods.
“…Specifically, SMC using ESO realizes voltage signals estimation for three‐phase two‐level power converters 12 . To the UAV system, 13 the SMC controller combines ESO to obtain the velocities and angular velocities signals to track the objective trajectory. Although ESO has been widely used in several applications to estimate the unknown states even the external disturbances, the disturbances signals in these complex nonlinear systems is deterministic.…”
This article presents sliding mode tracking control using finite-time nonlinear differentiator (FND) to the high-orders nonlinear systems that states are unknown and the output measurement signals involves stochastic disturbances. The FND using singular perturbation technique is applied to estimate the unknown states in the tracking system, and not rely on the model information under the condition of output stochastic signals. The stochastic noises involved in the output measurement signals are restrained sufficiently by the FNDs. The design of sliding mode tracking controller using FND reduces the chattering phenomenon efficiently. The analysis of systems stability and differentiator robustness is demonstrated. The comparative simulation results show that the sliding mode controller using FND track the desired trajectory in high accuracy with tracking errors fast convergence.
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