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This paper proposes a fault-tolerant control strategy based on a tilt-rotor quadcopter prototype, utilizing nonlinear model predictive control to maintain both attitude and position stability in the event of rotor failure. The control…

系统与控制 · 电气工程与系统科学 2025-11-10 Yanchao Wang , Xu You , Mehdi Baghdadi

This paper proposes a geometric adaptive controller for a quadrotor unmanned aerial vehicle with artificial neural networks. It is assumed that the dynamics of a quadrotor is disturbed by arbitrary, unstructured forces and moments caused by…

最优化与控制 · 数学 2019-03-07 Mahdis Bisheban , Taeyoung Lee

This paper presents a nonlinear control design for highly underactuated balance robots, which possess more numbers of unactuated degree-of-freedom (DOF) than actuated ones. To address the challenge of simultaneously trajectory tracking of…

机器人学 · 计算机科学 2023-10-03 Feng Han , Jingang Yi

Quadrotors are one of the popular unmanned aerial vehicles (UAVs) due to their versatility and simple design. However, the tuning of gains for quadrotor flight controllers can be laborious, and accurately stable control of trajectories can…

机器人学 · 计算机科学 2022-03-29 Vu Phi Tran , M. A Mabrok , Sreenatha G. Anavatti , Matthew A. Garratt , Ian R. Petersen

This paper presents the design of Variable-Pitch-Propeller mechanism and its application on a quadcopter called Heliquad to demonstrate its unique capabilities. The input-output relationship is estimated for a generic mechanism. Various…

系统与控制 · 电气工程与系统科学 2024-04-09 Eeshan Kulkarni , Suresh Sundaram

This paper presents the design of a geometric trajectory tracking controller for the cooperative task of two quadrotor UAVs (unmanned aerial vehicles) carrying and transporting a rigid bar, which is attached to the quadrotors via inflexible…

最优化与控制 · 数学 2022-07-13 Jacob R. Goodman , Leonardo J. Colombo

Many of the existing works on quadrotor control address the trajectory tracking problem by employing a cascade design in which the translational and rotational dynamics are stabilized by two separate controllers. The stability of the…

系统与控制 · 电气工程与系统科学 2025-03-25 Mirko Leomanni , Alberto Dionigi , Francesco Ferrante , Paolo Valigi , Gabriele Costante

The quadrotor unmanned aerial vehicle is a great platform for control systems research as its nonlinear nature and under-actuated configuration make it ideal to synthesize and analyze control algorithms. After a brief explanation of the…

系统与控制 · 计算机科学 2016-02-09 Andrew Zulu , Samuel John

Quadcopters, as unmanned aerial vehicles (UAVs), have great potential in civil applications such as surveying, building monitoring, and infrastructure condition assessment. Quadcopters, however, are relatively sensitive to noises and…

系统与控制 · 计算机科学 2019-01-04 Van Truong Hoang , Ansu Man Singh , Manh Duong Phung , Quang Ha

Utilizing a servo to tilt each rotor transforms quadrotors from underactuated to overactuated systems, allowing for independent control of both attitude and position, which provides advantages for aerial manipulation. However, this…

机器人学 · 计算机科学 2024-08-26 Jinjie Li , Junichiro Sugihara , Moju Zhao

In this article, a novel combined aerial cooperative tethered carrying and path planning framework is introduced with a special focus on applications in confined environments. The proposed work is aiming towards solving the path planning…

This paper presents a novel method to attenuate large horizontal wind disturbance for a small-scale unmanned autonomous helicopter combining wind tunnel-based experimental data and a backstepping algorithm. Large horizontal wind disturbance…

系统与控制 · 计算机科学 2019-05-10 Xiaorui Zhu , Wenwu Zeng , Zexiang Li , Chunyang Zheng

Obstacle avoidance for unmanned aerial vehicles like quadrotors is a popular research topic. Most existing research focuses only on static environments, and obstacle avoidance in environments with multiple dynamic obstacles remains…

机器人学 · 计算机科学 2025-03-19 Xiyu Fan , Minghao Lu , Bowen Xu , Peng Lu

This study explores modeling and control for quadrotor acrobatics, focusing on executing flip maneuvers. Flips are an elegant way to deliver sensor probes into no-fly or hazardous zones, like volcanic vents. Successful flips require…

机器人学 · 计算机科学 2024-02-01 Saransh Jain , Yash Shethwala , Jnaneshwar Das

Micro Aerial Vehicles (MAVs) are limited in their operation outdoors near obstacles by their ability to withstand wind gusts. Currently widespread position control methods such as Proportional Integral Derivative control do not perform well…

机器人学 · 计算机科学 2022-01-14 Ewoud J. J. Smeur , Guido C. H. E. de Croon , Qiping Chu

Hybrid unmanned aircraft can significantly increase the potential of micro air vehicles, because they combine hovering capability with a wing for fast and efficient forward flight. However, these vehicles are very difficult to control,…

机器人学 · 计算机科学 2019-09-27 E. J. J. Smeur , M. Bronz , G. C. H. E. de Croon

It has recently been shown that all physical parameters of an Incremental Nonlinear Dynamic Inversion (INDI) controller can be estimated onboard a multirotor within half a second, which is fast enough to do the full identification during a…

机器人学 · 计算机科学 2026-05-08 Tom Aantjes , Till M. Blaha , Spilios Theodoulis , Ewoud J. J. Smeur

This paper applies the UAV to the inspection of water diversion pipelines in hydropower stations. The diversion pipeline is an enclosed space, so the airflow disturbance caused by the rotation of the UAV blades and the strong air convection…

系统与控制 · 电气工程与系统科学 2022-12-16 QuanXi Zhan , JunRui Zhang , ChenYang Sun , RunJie Shen , Bin He

Quadrotors that can operate predictably in the presence of imperfect model knowledge and external disturbances are crucial in safety-critical applications. We present L1Quad, a control architecture that ensures uniformly bounded transient…

系统与控制 · 电气工程与系统科学 2024-12-23 Zhuohuan Wu , Sheng Cheng , Pan Zhao , Aditya Gahlawat , Kasey A. Ackerman , Arun Lakshmanan , Chengyu Yang , Jiahao Yu , Naira Hovakimyan

This paper provides new results for control of complex flight maneuvers for a quadrotor unmanned aerial vehicle (UAV). The flight maneuvers are defined by a concatenation of flight modes or primitives, each of which is achieved by a…

最优化与控制 · 数学 2011-09-13 Taeyoung Lee , Melvin Leok , N. Harris McClamroch