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Relevant bibliographies by topics / UAV, quadrotor, embedded model control, feedback linearization

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Journal articles
Dissertations / Theses

Academic literature on the topic 'UAV, quadrotor, embedded model control, feedback linearization'

Author: Grafiati

Published: 14 March 2023

Last updated: 31 July 2025

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Journal articles on the topic "UAV, quadrotor, embedded model control, feedback linearization"

1

Lotufo, M. A., L. Colangelo, C. Perez-Montenegro, C. Novara, and E. Canuto. "Embedded Model Control for UAV Quadrotor via Feedback Linearization." IFAC-PapersOnLine 49, no. 17 (2016): 266–71. http://dx.doi.org/10.1016/j.ifacol.2016.09.046.

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2

Shao, Keyong, Wenjing Xia, Yujie Zhu, Chenjun Sun, and Yang Liu. "Research on UAV Trajectory Tracking Control System Based on Feedback Linearization Control–Fractional Order Model Predictive Control." Processes 13, no. 3 (2025): 801. https://doi.org/10.3390/pr13030801.

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Aiming at the problem of the nonlinear, strongly coupled, and underdriven trajectory tracking instability of a quadrotor unmanned aerial vehicle (UAV), this thesis proposes a feedback linearization and fractional order model predictive control strategy based on feedback linearization by modeling the dynamics of the UAV control system and linearizing the nonlinear model of attitude control. A dual closed-loop control structure, feedback linearization control (FLC) for a position loop, and fractional order model predictive control (FOMPC) for an attitude loop are adopted to realize fast position

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3

Yuan, Xingyu, Jinfa Xu, and Shengwei Li. "Design and Simulation Verification of Model Predictive Attitude Control Based on Feedback Linearization for Quadrotor UAV." Applied Sciences 15, no. 9 (2025): 5218. https://doi.org/10.3390/app15095218.

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The flight dynamics of quadrotor UAVs are characterized by significant nonlinearity and inter-axis coupling, posing challenges for the direct application of linear control theory in flight control system design. This paper proposes a feedback linearization transformation method to reduce the computational burden of MPC while addressing the nonlinear coupled flight dynamics in attitude control. The quadrotor UAV’s attitude motion is transformed via feedback linearization into a linear decoupled model, consisting of three independent second-order systems. MPC theory is then employed to design th

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4

Hoshu, Ayaz Ahmed, Ghulam E. Mustafa Abro, Musaed Alhussein, Irfan Ali Tunio, Khursheed Aurangzeb, and Anwar Ali. "Cascaded Control System Design for Quadrotor UAV through Relay with Embedded Integrator-Based Automatic Tuning Approach." International Journal of Aerospace Engineering 2023 (October 10, 2023): 1–10. http://dx.doi.org/10.1155/2023/6651286.

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Due to their enormous characteristics and applicability, quadrotor unmanned aerial vehicles (UAVs) have enjoyed much popularity lately. However, designing a stable control strategy for quadrotors still remains one of the major concerns mainly due to the requirement of an accurate system model. They are naturally underactuated systems, with complex and nonlinear dynamics as well as interaxes couplings. Considering the dynamical complexities of these vehicles, one of the efficient methods is to utilize the relay feedback experiments and automatic tuning approach to tackle these issues. This pape

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5

Rinaldi, Marco, Stefano Primatesta, and Giorgio Guglieri. "A Comparative Study for Control of Quadrotor UAVs." Applied Sciences 13, no. 6 (2023): 3464. http://dx.doi.org/10.3390/app13063464.

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Modeling and controlling highly nonlinear, multivariable, unstable, coupled and underactuated systems are challenging problems to which a unique solution does not exist. Modeling and control of Unmanned Aerial Vehicles (UAVs) with four rotors fall into that category of problems. In this paper, a nonlinear quadrotor UAV dynamical model is developed with the Newton–Euler method, and a control architecture is proposed for 3D trajectory tracking. The controller design is decoupled into two parts: an inner loop for attitude stabilization and an outer loop for trajectory tracking. A few attitude sta

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6

Khalid, Adnan, Zohaib Mushtaq, Saad Arif, Kamran Zeb, Muhammad Attique Khan, and Sambit Bakshi. "Control Schemes for Quadrotor UAV: Taxonomy and Survey." ACM Computing Surveys, September 8, 2023. http://dx.doi.org/10.1145/3617652.

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Quadrotor Unmanned Aerial Vehicle (UAV) is an unstable system so it needs to be controlled efficiently and intelligently. Moreover, due to its non-linear, coupled, and under-actuated nature, the quadrotor has become an important research platform to study and validate various control theories. Different control approaches have been used to control the quadrotor UAV. In this context, a comprehensive study of different control schemes is presented in this research. First, an overview of the working and different applications of quadrotor UAVs is presented. Secondly, a mathematical model of the q

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7

Ghasemi, Ali, Farhad Parivash, and Serajeddin Ebrahimian. "Autonomous landing of a quadrotor on a moving platform using vision-based FOFPID control." Robotica, September 20, 2021, 1–19. http://dx.doi.org/10.1017/s0263574721001181.

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Abstract This research deals with the autonomous landing maneuver of a quadrotor unmanned aerial vehicle (UAV) on an unmanned ground vehicle (UGV). It is assumed that the UGV moves independently, and there is no communication and collaboration between the two vehicles. This paper aims at the design of a closed-loop vision-based control system for quadrotor UAV to perform autonomous landing maneuvers in the possible minimum time despite the wind-induced disturbance force. In this way, a fractional-order fuzzy proportional-integral-derivative controller is introduced for the nonlinear under-actu

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8

Singh, Brajesh Kumar, and Awadhesh Kumar. "Model predictive control using LPV approach for trajectory tracking of quadrotor UAV with external disturbances." Aircraft Engineering and Aerospace Technology, October 5, 2022. http://dx.doi.org/10.1108/aeat-12-2021-0368.

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Purpose The rotorcraft technology is very interesting area since last few decades due to variety of applications. One of the rotorcrafts is the quadrotor unmanned aerial vehicle (QUAV), which contains four rotors mounted on an airframe with an onboard controller. The QUAV is a highly nonlinear system and underactuated. Its controller design is very challenging task, and the need of controller is to make it autonomous based on mission planning. The purpose of this study is to design a controller for quadrotor UAV for attitude stabilization and trajectory tracking problem in presence of external

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Dissertations / Theses on the topic "UAV, quadrotor, embedded model control, feedback linearization"

1

LOTUFO, MAURICIO ALEJANDRO. "Embedded Model Control for UAVs: theoretical aspects, simulations and experimental results." Doctoral thesis, Politecnico di Torino, 2017. http://hdl.handle.net/11583/2687427.

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Unmanned Aerial Vehicles (UAVs) and, more specifically, n-copters have come to prominence in the last decade. Indeed, unmanned vehicles may have several applications in society, spanning from complex operations, also in potentially hazardous environments for humans to more entertaining purposes. Furthermore, UAVs have drawn great attention in the automatic control research community. This is mainly due to two reasons. First of all, designing a control for this non-linear and underactuated system can represent a stimulating challenge for control researchers. Secondly, n-copters, being ty

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