Relevant bibliographies by topics / Quadrotor Software Design

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  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Quadrotor Software Design'

Author: Grafiati
Published: 4 June 2021
Last updated: 5 February 2022

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Journal articles on the topic "Quadrotor Software Design"

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Huang, Z. W., Z. Chen, B. P. Bian, and Y. Tang. "Design of Quadrotor Helicopter Based on STM32." Applied Mechanics and Materials 644-650 (September 2014): 790–93. http://dx.doi.org/10.4028/www.scientific.net/amm.644-650.790.

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Quadrotor helicopter is light and very agile aerial robots which attracted much attention of scientists. A practical implementation of a quadrotor helicopter based on STM32 is described in this article, applying MPU6050 and other inertial sensors. The hardware structures and software flow chart of flight control are both presented. The discussions with the key problems during the process of implementation are also made.
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Wang, Hanzhang, and Yisha Liu. "A low-cost autonomous navigation system for a quadrotor in complex outdoor environments." International Journal of Advanced Robotic Systems 17, no. 1 (2020): 172988142090515. http://dx.doi.org/10.1177/1729881420905150.

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In this article, we design a low-cost navigation system for a quadrotor working in unknown outdoor environments. To reduce the computing burden of the quadrotor, we build a separated system and transfer the computing resources from onboard side to ground station side. Both sides’ communication is guaranteed by 5G wireless networks. We utilize a stereo camera to acquire point clouds and build Octomap for the quadrotor’s navigation. Then, the trajectory is generated in two stages. In the first stage, a modified RRT*-CONNECT algorithm is adopted to generate a set of collision-free waypoints. In t
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Xiaochen Dong, and Fei Yan. "Design of Attitude Control System for Quadrotor." International Journal of Digital Content Technology and its Applications 7, no. 5 (2013): 350–57. http://dx.doi.org/10.4156/jdcta.vol7.issue5.42.

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Benbouali, Abderrahmen, Fayçal Chabni, Rachid Taleb, and Noureddine Mansour. "Flight parameters improvement for an unmanned aerial vehicle using a lookup table based fuzzy PID controller." Indonesian Journal of Electrical Engineering and Computer Science 23, no. 1 (2021): 171. http://dx.doi.org/10.11591/ijeecs.v23.i1.pp171-178.

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In this paper, a control scheme based on lookup table fuzzy proportionalintegral-derivate (PID) controller for the quadrotor unmanned aerial vehicle (UAV) movement control is proposed. This type of control provides enhanced quadrotor movement control beyond what can be achieved with conventional controllers and has a less computational burden on the processor. The proposed control scheme uses three lookup table based fuzzy logic controllers to control the different movement ranges of a quadrotor (i.e. roll, pitch, and yaw) to achieve stability. The mathematical model of a quadrotor, used to de
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Huang, Sibo, Jianfeng Huang, Zhaoquan Cai, and Han Cui. "Adaptive Backstepping Sliding Mode Control for Quadrotor UAV." Scientific Programming 2021 (September 13, 2021): 1–13. http://dx.doi.org/10.1155/2021/3997648.

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Quadrotor UAV has a strong mobility and flexibility in flight and has been widely used in military and civil fields in recent years. An adaptive backstepping sliding mode control (ABSMC) method is proposed to address the trajectory tracking control problem of quadrotor UAV based on actuator fault and external disturbance. In the proposed method, the switching gain of adaptive sliding mode control is constructed in the backstepping design process in order to suppress the chattering effect of sliding mode control effectively by differential iteration. Firstly, the dynamic model of quadrotor UAV
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Lasmadi, Lasmadi. "Sistem Navigasi Quadrotor Berbasis IMU dengan Kalman Filter." ELKHA 11, no. 1 (2019): 39. http://dx.doi.org/10.26418/elkha.v11i1.30502.

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The navigation system on quadrotor is important to maintain stability and determine its own position when flying autonomously. The GPS can provide the position measurement, but it has limitations in the specific environments and cannot provide the orientation information. This study aims to design the navigation system for quadrotor based on IMU sensor with Kalman filters using the state space model. The system model was developed using Matlab software. Kalman filter is designed to estimate the navigation data and eliminate noise on the sensor so that it can improve the measurement accuracy. T
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Abro, Ghulam E. Mustafa, Saiful Azrin B. M. Zulkifli, Vijanth Sagayan Asirvadam, and Zain Anwar Ali. "Model-Free-Based Single-Dimension Fuzzy SMC Design for Underactuated Quadrotor UAV." Actuators 10, no. 8 (2021): 191. http://dx.doi.org/10.3390/act10080191.

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The underactuated quadrotor unmanned aerial vehicle (UAV) is one of the nonlinear systems that have few actuators as compared to the degree of freedom (DOF); thus, it is a strenuous task to stabilize its attitude and positions. Moreover, an induction of unmodelled dynamic factors and uncertainties make it more difficult to control its maneuverability. In this paper, a model-free based single-dimension fuzzy sliding mode control (MFSDF-SMC) is proposed to control the attitude and positions of underactuated quadrotor UAV. The paper discusses the kinematic and dynamic models with unmodelled dynam
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Boudjit, Kamel, Cherif Larbes, and Naeem Ramzan. "ANN design and implementation for real-time object tracking using quadrotor AR.Drone 2.0." Journal of Experimental & Theoretical Artificial Intelligence 30, no. 6 (2018): 1013–35. http://dx.doi.org/10.1080/0952813x.2018.1509896.

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Badr, Sherif, Omar Mehrez, and A. E. Kabeel. "A design modification for a quadrotor UAV: modeling, control and implementation." Advanced Robotics 33, no. 1 (2018): 13–32. http://dx.doi.org/10.1080/01691864.2018.1556116.

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Chu, Zhaobi, Songgang Zhou, Min Zhu, and Hua Li. "Finite-time trajectory control for a quadrotor aircraft using disturbance observer." International Journal of Advanced Robotic Systems 17, no. 2 (2020): 172988142090384. http://dx.doi.org/10.1177/1729881420903847.

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In this article, we investigate the problem of finite-time trajectory tracking control for a quadrotor aircraft with unknown external disturbances. To improve convergence rate and disturbance rejection performance, a new composite controller is proposed by integrating finite-time control design and disturbance estimation attenuation technique. Explicit Lyapunov function is given to ensure the finite-time stability of the closed-loop control system. Numerical simulations also show the effectiveness of the proposed method.
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Dissertations / Theses on the topic "Quadrotor Software Design"

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"Modeling, Control and Design of a Quadrotor Platform for Indoor Environments." Master's thesis, 2018. http://hdl.handle.net/2286/R.I.51763.

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abstract: Unmanned aerial vehicles (UAVs) are widely used in many applications because of their small size, great mobility and hover performance. This has been a consequence of the fast development of electronics, cheap lightweight flight controllers for accurate positioning and cameras. This thesis describes modeling, control and design of an oblique-cross-quadcopter platform for indoor-environments. One contribution of the work was the design of a new printed-circuit-board (PCB) flight controller (called MARK3). Key features/capabilities are as follows: (1) a Teensy 3.2 microcontroller w
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Book chapters on the topic "Quadrotor Software Design"

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A. Rendón, Manuel. "Quadrotor Unmanned Aerial Vehicles: Visual Interface for Simulation and Control Development." In Robotics Software Design and Engineering. IntechOpen, 2021. http://dx.doi.org/10.5772/intechopen.97435.

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Quadrotor control is an exciting research area. Despite last years developments, some aspects demand a deeper analysis: How a quadrotor operates in challenging trajectories, how to define trajectory limits, or how changing physical characteristics of the device affects the performance. A visual interface development platform is a valuable tool to support this effort, and one of these tools is briefly described in this Chapter. The quadrotor model uses Newton-Euler equations with Euler angles, and considers the effect of air drag and propellers’ speed dynamics, as well as measurement noise and limits for propeller speeds. The tool is able to test any device just by setting a few parameters. A three-dimensional optimal trajectory defined by a set of waypoints and corresponding times, is calculated with the help of a Minimum Snap Trajectory planning algorithm. Small Angle Control, Desired Thrust Vector (DTV) Control and Geometric Tracking Control are the available strategies in the tool for quadrotor attitude and trajectory following control. The control gains are calculated using Particle Swarm Optimization. Root Mean Square (RMS) error and Basin of Attraction are employed for validation. The tool allows to choose the control strategy by visual evaluation on a graphical user interface (GUI), or analyzing the numerical results. The tool is modular and open to other control strategies, and is available in GitHub.
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Conference papers on the topic "Quadrotor Software Design"

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Yao, Ming, and Yunqing Xu. "Design of Nonlinear Aero Controller and Simulation for Quadrotor Unmanned Aerial Vehicles." In 2013 Fourth World Congress on Software Engineering (WCSE). IEEE, 2013. http://dx.doi.org/10.1109/wcse.2013.52.

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Silano, Giuseppe, Pasquale Oppido, and Luigi Iannelli. "Software-in-the-loop simulation for improving flight control system design: a quadrotor case study." In 2019 IEEE International Conference on Systems, Man and Cybernetics (SMC). IEEE, 2019. http://dx.doi.org/10.1109/smc.2019.8914154.

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Yao, Yi, Zhicheng Deng, Xiaoqing Zhang, and Chao Lv. "Design of a Quadrotor Control Software Experimental Validation Platform Based on Real-Time Hardware-in-the-Loop Simulation." In 2021 10th International Conference on Educational and Information Technology (ICEIT). IEEE, 2021. http://dx.doi.org/10.1109/iceit51700.2021.9375598.

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Journal articles
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