2017
DOI: 10.1177/0954410017703414
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Receding horizon control of a 3 DOF helicopter using online estimation of aerodynamic parameters

Abstract: This study presents a numerical implementation of fast nonlinear model predictive control (NMPC) and nonlinear moving horizon estimation (NMHE) for the trajectory tracking problem of a 3 degree of freedom (DOF) helicopter. The motivation behind using the NMPC instead of its linear counterpart is that the helicopter is operated over nonlinear regions. Moreover, this system has cross-couplings that make the control of the system even more complicated. What is more, according to our simulation scenario, the syste… Show more

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Cited by 18 publications
(13 citation statements)
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“…In the lateral cascade channel, the lateral offset reference, y c , is the reference input of the y lateral offset channel, and the intermediate variable, c , is regarded as the reference input of the roll angle, , channel. From the lateral state equations (17) and (18), the relative equations can be rewritten as…”
Section: Control Lawmentioning
confidence: 99%
See 1 more Smart Citation
“…In the lateral cascade channel, the lateral offset reference, y c , is the reference input of the y lateral offset channel, and the intermediate variable, c , is regarded as the reference input of the roll angle, , channel. From the lateral state equations (17) and (18), the relative equations can be rewritten as…”
Section: Control Lawmentioning
confidence: 99%
“…Second, the required calculation time and the computing resources available on autopilot inhibit these optimization solutions. In Papachristos et al., 12,13 Alexis et al., 14 Kamel et al., 15 Liu et al., 16 and Mehndiratta and Kayacan, 17 a powerful model predictive control method was designed to deal with the issues of path tracking based on commercial autopilot for thrust-vectoring of a TTR–UAV, but the method’s calculation cost can prove prohibitive. The UAV proposed in Fang et al.…”
Section: Introductionmentioning
confidence: 99%
“…Many difficulties have been arrived to design suitable control algorithms for unmanned helicopter due to its high nonlinearity, inter‐axis cross‐coupling, unstable system dynamics, and parametric uncertainty during the last two decades 3‐5 . Active research is continuing to develop controllers for UAVs, which can work successfully in spite of all difficulties 5‐7 …”
Section: Introductionmentioning
confidence: 99%
“…Recently, a learning‐based model predictive control (LBMPC) technique has been developed in Reference 20, where a modified extended Kalman filter (EKF) is used to perform state estimation and learn updated model parameters. Whereas, in References 7,21‐23, a nonlinear moving horizon estimation has been used for nonlinear system to improve the performance of LBMPC.…”
Section: Introductionmentioning
confidence: 99%
“…During the past decades, considerable research and increasing attention have been done on the design, analysis, and operation of the unmanned autonomous helicopters (UAHs) due to their widely application prospects in the field of military and civilian. [1][2][3] However, unlike other mechanical systems, the UAHs are special controlled objects with the characters of underactuation, multivariate, strong coupling and nonlinearity. 4 Especially for the medium-scale UAHs, who possess the merits of fast speed, high altitude, long cruise and large payload compared with the small-scale UAHs, it is still a challenge to design effective and robust controller for them.…”
Section: Introductionmentioning
confidence: 99%