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Relevant bibliographies by topics / Quadrotor MAV

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Academic literature on the topic 'Quadrotor MAV'

Author: Grafiati

Published: 4 June 2025

Last updated: 1 August 2025

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Journal articles on the topic "Quadrotor MAV"

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Lei, Yao, Yiyong Huang, and Hengda Wang. "Effects of Wind Disturbance on the Aerodynamic Performance of a Quadrotor MAV during Hovering." Journal of Sensors 2021 (April 21, 2021): 1–13. http://dx.doi.org/10.1155/2021/6681716.

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Wind disturbance could render thrust and power variation or even causing roll which is difficult to maintain a steady flight in gust especially when the horizontal or vertical wind is involved. In this paper, the horizontal wind and vertical wind are presented to study the influence of wind disturbance on aerodynamic characteristics of the quadrotor aircraft in hovering by experiments and numerical simulations. First, the simplified aerodynamic model with the wind disturbance was analyzed in detail. Also, the low-speed wind tunnel tests were performed to obtain the thrust and power variation o

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Noordin, A., M. A. M. Basri, and Z. Mohamed. "Simulation and experimental study on PID control of a quadrotor MAV with perturbation." Bulletin of Electrical Engineering and Informatics 9, no. 5 (2020): 1811–18. http://dx.doi.org/10.11591/eei.v9i5.2158.

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This paper presents a proportional-integral-derivative (PID) flight controller for a quadrotor micro air vehicle (MAV). The MAV (Parrot Mambo minidrones) is small, therefore, a slight perturbation will affect its performance. Hence, for the actuated dynamics, roll (ϕ), pitch (θ), yaw (ψ), and z stabilization, a PID control scheme is proposed. Furthermore, the same controller technique is also applied for under-actuated dynamics x and y position control. The newtonian model is simulated using simulink with a normal Gaussian noise of force as external disturbances. using simulink support package

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A., Noordin, A. M. Basri M., and Mohamed Z. "Simulation and experimental study on PID control of a quadrotor MAV with perturbation." Bulletin of Electrical Engineering and Informatics 9, no. 5 (2020): 1811–18. https://doi.org/10.11591/eei.v9i5.2158.

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This paper presents a proportional-integral-derivative (PID) flight controller for a quadrotor micro air vehicle (MAV). The MAV (Parrot Mambo minidrones) is small, therefore, a slight perturbation will affect its performance. Hence, for the actuated dynamics, roll (ϕ), pitch (θ), yaw (ψ), and z stabilization, a PID control scheme is proposed. Furthermore, the same controller technique is also applied for under-actuated dynamics x and y position control. The newtonian model is simulated using simulink with a normal Gaussian noise of force as external disturbances. using simulink suppo

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Yadav, Indrajeet, Michael Sebok, and Herbert G. Tanner. "Receding horizon navigation and target tracking for aerial detection of transient radioactivity." International Journal of Robotics Research 42, no. 3 (2023): 66–82. http://dx.doi.org/10.1177/02783649231169803.

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The paper presents a receding horizon planning and control strategy for quadrotor-type micro aerial vehicle (mav)s to navigate reactively and intercept a moving target in a cluttered unknown and dynamic environment. Leveraging a lightweight short-range sensor that generates a point-cloud within a relatively narrow and short field of view (fov), and an ssd-MobileNet based Deep neural network running on board the mav, the proposed motion planning and control strategy produces safe and dynamically feasible mav trajectories within the sensor fov, which the vehicle uses to autonomously navigate, pu

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Bouchaib, Ali, Rachid Taleb, Abderrahmen Benbouali, Taieb Bessaad, and Hemza Saidi. "High dynamic performance based by sliding mod control of quadrotor MAV." STUDIES IN ENGINEERING AND EXACT SCIENCES 5, no. 2 (2024): e8988. http://dx.doi.org/10.54021/seesv5n2-318.

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The paper focuses on strong control of high dynamic performance based on the sliding mode in order to control the quadrotor MAV. The model used in the simulation is the Newton-Euler model, and also choose the Mambo Parrot quadrotor parameters, to improve the latter's performance in terms of accuracy and robustness in case the impedance control chosen by the manufacturer needs to be changed. The results of which gave effectiveness and efficiency compared to classical controls PID and sliding mode. High dynamic performance control (HDP) is a type of control system designed to provide the highest

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Briliauskas, Mantas. "Learning Stabilization Control of Quadrotor in Near-Ground Setting Using Reinforcement Learning." Information Technology and Control 53, no. 1 (2024): 237–42. http://dx.doi.org/10.5755/j01.itc.53.1.35135.

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With the development of intelligent systems, the popularity of using micro aerial vehicles (MAV) increases significantly in the fields of rescue, photography, security, agriculture, and warfare. New modern solutions of machine learning like ChatGPT that are fine-tuned using reinforcement learning (RL) provides evidence of new trends in seeking general artificial intelligence. RL has already been proven to work as a flight controller for MAV performing better than Proportional Integral Derivative (PID)-based solutions. However, using negative Euclidean distance to the target point as the reward

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Lei, Yao, and Hengda Wang. "Aerodynamic Performance of a Quadrotor MAV Considering the Horizontal Wind." IEEE Access 8 (2020): 109421–28. http://dx.doi.org/10.1109/access.2020.3002706.

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Cheng, Xiaoqi, Xinfeng Liang, Xiaosong Li, Zhimin Liu, and Haishu Tan. "Autonomous Landing Strategy for Micro-UAV with Mirrored Field-of-View Expansion." Sensors 24, no. 21 (2024): 6889. http://dx.doi.org/10.3390/s24216889.

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Positioning and autonomous landing are key technologies for implementing autonomous flight missions across various fields in unmanned aerial vehicle (UAV) systems. This research proposes a visual positioning method based on mirrored field-of-view expansion, providing a visual-based autonomous landing strategy for quadrotor micro-UAVs (MAVs). The forward-facing camera of the MAV obtains a top view through a view transformation lens while retaining the original forward view. Subsequently, the MAV camera captures the ground landing markers in real-time, and the pose of the MAV camera relative to

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Li, Yamin, Bowen Sun, Ping Xia, and Yang Yang. "Energy-Optimal 3D Path Planning for MAV with Motion Uncertainty." Complexity 2021 (October 18, 2021): 1–6. http://dx.doi.org/10.1155/2021/9994680.

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Practical applications of microaerial vehicle face significant challenges including imprecise localization, limited on-board energy, and motion uncertainty. This paper focuses on the latter two issues. The core of proposed energy-optimal path planning algorithm is an energy consumption model deriving from real measurements of a specific quadrotor and utilizing a 2D Gaussian distribution function to simulate the uncertainty of random drift. Based on these two models, we formulate the optimal path traversing the 3D map with minimum energy consumption using a heuristic ant colony optimization. Mu

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Noordin, Aminurrashid, Mohd Ariffanan Mohd Basri, and Zaharuddin Mohamed. "Position and Attitude Tracking of MAV Quadrotor Using SMC-Based Adaptive PID Controller." Drones 6, no. 9 (2022): 263. http://dx.doi.org/10.3390/drones6090263.

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A micro air vehicle (MAV) is physically lightweight, such that even a slight perturbation could affect its attitude and position tracking. To attain better autonomous flight system performance, MAVs require good control strategies to maintain their attitude stability during translational movement. However, the available control methods nowadays have fixed gain, which is associated with the chattering phenomenon and is not robust enough. To overcome the aforementioned issues, an adaptive proportional integral derivative (PID) control scheme is proposed. An adaptive mechanism based on a second-o

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Dissertations / Theses on the topic "Quadrotor MAV"

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Gilson, Maximillian Andrew. "Fault-tolerant mapping and localization for Quadrotor UAV." Wright State University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright157865858408435.

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Ericson, Ludvig. "Flying High: Deep Imitation Learning of Optimal Control for Unmanned Aerial Vehicles." Thesis, KTH, Robotik, perception och lärande, RPL, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-233326.

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Optimal control for multicopters is difficult in part due to the low processing power available, and the instability inherent to multicopters. Deep imitation learning is a method for approximating an expert control policy with a neural network, and has the potential of improving control for multicopters. We investigate the performance and reliability of deep imitation learning with trajectory optimization as the expert policy by first defining a dynamics model for multicopters and applying a trajectory optimization algorithm to it. Our investigation shows that network architecture plays an imp

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Sobers, David Michael Jr. "Efficient ranging-sensor navigation methods for indoor aircraft." Diss., Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/34824.

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Unmanned Aerial Vehicles are often used for reconnaissance, search and rescue, damage assessment, exploration, and other tasks that are dangerous or prohibitively difficult for humans to perform. Often, these tasks include traversing indoor environments where radio links are unreliable, hindering the use of remote pilot links or ground-based control, and effectively eliminating Global Positioning System (GPS) signals as a potential localization method. As a result, any vehicle capable of indoor flight must be able to stabilize itself and perform all guidance, navigation, and control tasks with

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Burkamshaw, Leon Keith. "Towards a low-cost quadrotor research platform." Monterey, California : Naval Postgraduate School, 2010. http://edocs.nps.edu/npspubs/scholarly/theses/2010/Mar/10Mar%5FBurkamshaw.pdf.

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Thesis (M.S. in Software Engineering)--Naval Postgraduate School, March 2010.<br>Thesis Advisor(s): Horner, Douglas. Second Reader: Michael James B. "March 2010." Description based on title screen as viewed on April 27, 2010. Author(s) subject terms: Rapid application development, quadrotor helicopter, quadcopter, inertial measurement unit, digital signal processing, Nintendo Wii Motionplus, dsPIC. Includes bibliographical references (p. 65-66). Also available in print.

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Book chapters on the topic "Quadrotor MAV"

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Noordin, Aminurrashid, Mohd Ariffanan Mohd Basri, Zaharuddin Mohamed, and Izzuddin Mat Lazim. "Attitude and Altitude Control of Quadrotor MAV using FOPID Controller." In Communications in Computer and Information Science. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-7243-2_9.

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Mehta, Ankur M., Daniela Rus, Kartik Mohta, Yash Mulgaonkar, Matthew Piccoli, and Vijay Kumar. "A Scripted Printable Quadrotor: Rapid Design and Fabrication of a Folded MAV." In Springer Tracts in Advanced Robotics. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-28872-7_12.

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Noordin, Aminurrashid, Mohd Ariffanan Mohd Basri, Zaharuddin Mohamed, and Izzuddin Mat Lazim. "Position and Attitude Control of Quadrotor MAV Using Sliding Mode Control with Tanh Function." In Enabling Industry 4.0 through Advances in Mechatronics. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2095-0_18.

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Arbery, Glenn Cannon. "Victims of Likeness: Quadroons and Octoroons in Southern Fiction *." In Interracialism. Oxford University PressNew York, NY, 2000. http://dx.doi.org/10.1093/oso/9780195128567.003.0023.

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Abstract At certain junctures since the mid-nineteenth century, American fiction about the antebellum South has explored the relations between the races, especially in matters of equality, by dwelling with fascination and perplexity on the enigmatic figure of the quadroon or the octoroon. The words themselves, now rather arcane, are liable to evoke the image of “a face like a tragic magnolia, the eternal female, the eternal Who-suffers”-Faulkner’s description of Charles Hon’s mistress in Absalom, Absalom! Derived from the Spanish cuarteron, “quadroon” denoted a person one-fourth black, that is

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Low, Matthew, Timothy E. Wang, and Pierluigi Nuzzo. "Learning Compositional, Time-Varying Neural Barrier Contracts." In Frontiers in Artificial Intelligence and Applications. IOS Press, 2024. http://dx.doi.org/10.3233/faia240640.

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Certificate functions can be used to efficiently capture and prove various properties of a system or controller. Control barrier functions (CBFs) are certificate functions that define a region of forward-invariance, which makes them a natural choice to enforce a notion of “safety” for a system. However, synthesizing CBFs, especially in the case of complex systems with learning-enabled components, remains a challenge. Recent work achieves promising results by leveraging neural networks as function approximators to learn CBFs. However, a single CBF may not exist or be difficult to obtain for com

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Conference papers on the topic "Quadrotor MAV"

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Solomon, Eric, Vikram Hrishikeshavan, and Inderjit Chopra. "Autonomous Quadrotor Control and Navigation with Snapdragon Flight." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12911.

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Visual-inertial odometry has demonstrated the ability to turn a traditional micro-aerial vehicle (MAV) into an advanced platform for aerial robotics. Traditional MAV platforms suffer from strict weight limitations and in some cases flight controllability issues. Qualcomm's Snapdragon Flight™ is utilized to solve both of these problems. It is chosen due to its low weight and high processing power. Results show sufficient controllability to conclude feasibility using Snapdragon Flight™ in GPS-denied environments and onboard unconventional MAV frames. This study is presented with a generic quadro

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Haviland, Stephen, Dmitry Bershadsky, Daniel Magree, and Eric Johnson. "Development of a 500 gram Vision-based Autonomous Quadrotor Vehicle Capable of Indoor Navigation." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10295.

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This paper presents the work and related research done in preparation for the American Helicopter Society (AHS) Micro Aerial Vehicle (MAV) Student Challenge. The described MAV operates without human interaction in search of a ground target in an open indoor environment. The Georgia Tech Quadrotor-Mini (GTQ-Mini) weighs under 500 grams and was specifically sized to carry a high processing computer. The system platform also consists of a monocular camera, sonar, and an inertial measurement unit (IMU). All processing is done onboard the vehicle using a lightweight powerful computer. A vision navi

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Hu, Botao, and Sandipan Mishra. "Time-optimal Trajectory Planning for Landing Onto Moving Platforms." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12203.

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In this paper, an algorithm for time-optimal trajectory generation is developed for landing a 6 degree-of-freedom (DOF) quadrotor onto a moving platform (with tilt, heave and pitch). The overall control architecture has a standard guidance-and-tracking control inner-outer loop structure. The outer loop (guidance control) solves the time-optimal trajectory generation problem. Instead of directly solving the time-optimal control problem, the proposed method reformulates this into a nonlinear programming problem that transforms the constraints on the original system dynamics and inputs onto const

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Kottapalli, Sesi, and Douglas Boyd, Jr. "Follow-on Study on the Applicability of Fly Neighborly Noise Recommendations to UAM Quadrotors in Steady Maneuvers." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-53.

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A follow-on study to the 2024 paper by Kottapalli, Silva, and Boyd is presented with improved acoustics tools to examine whether the Vertical Aviation International (VAI) Fly Neighborly operational recommendations that are designed for single main rotor/tail rotor configurations will hold for non-conventional UAM rotorcraft with multiple rotors. The 6-occupant quadrotor concept vehicle designed under the NASA Revolutionary Vertical Lift Technology (RVLT) Project is studied. The tip speed is 550 ft/sec, with three blades per rotor. Predictions are made for three steady maneuvers: level turns, d

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Vemprala, Sai, and Srikanth Saripalli. "Vision based Collaborative Localization for Swarms of Aerial Vehicles." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12204.

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We present a framework for localizing a swarm of multirotor micro aerial vehicles (MAV) through collaboration using vision based sensing. For MAVs equipped with monocular cameras, this technique, built upon a relative pose estimation strategy between two or more cameras, enables the MAVs to share information of a common map and thus estimate accurate metric poses between each other even through fast motion and changing environments. Synchronized feature detection, matching and robust tracking enable the use of multiple view geometry concepts for performing the estimation. Furthermore, we prese

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Gautam, Alvika, P. B. Sujit, Ashwini Ratnoo, and IIIT-Delhi; Saripalli. "Robust Autonomous Landing of a Quadrotor on a Moving Target." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12908.

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Autonomous landing is the most difficult maneuver in a quadrotor mission because of challenges like (i) external disturbances and localization error both of which cause deviation from the desired trajectory and may result in a crash. In this paper, we use onboard vision to detect and estimate the landing target parameters accurately. We present a guidance framework to land on a moving target accurately. We discuss the advantages and present the simulation results for a simple 2D scenario for the proposed framework. We present implementation of the proposed algorithm for a quadrotor vehicle sim

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Arace, Matt, and Anubhav Datta. "Impact of Detailed SFC on Hybrid-Electric VTOL Sizing." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1341.

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Data from a 3.43 kW piston engine-generator is integrated with rotorcraft sizing analysis to assess its impact. First, the measured SFC map of the powerplant is modeled. Second, the sizing is validated with XV-15 flight test aircraft and NASA conceptual reference quadrotor. The power and platform models are then integrated to size a hypothetical quadrotor bi-plane unmanned air vehicle of 5 lb payload. Several cases for how the engine can be operated to meet the vehicle torque and speed are detailed. The key conculsion is that a detailed SFC model is as important as the aircraft model. Without

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Crane, Jason, and Imraan Faruque. "Testing and Characterization of Hybrid Unmanned Aerial/Underwater Vehicle at the air-water interface." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12205.

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Hybrid Unmanned Aerial/Underwater Vehicles (HUA/UV's) have the challenge of robustly operating within and transitioning between two vastly different environments. To meet this challenge, an amphibious quadrotor was constructed and its transition performance quantified using motion capture under manual control. The approach is novel in that it performs transition without active buoyancy control or increasing the number of rotors. The loads across air-water transition were quantified using a controlled single motor-propeller pod and a six-axis load cell. Experimental results were compared agains

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Goli, Nishanth, David Arterburn, Chris Duling, and Chris Sallis. "Modeling and Simulation of sUAS Impact Characteristics Following In-Flight Failures." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12912.

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The injury potential to a human from a descending small Unmanned Aerial System (sUAS) following an in-flight failure has a large impact on how the FAA chooses to regulate sUAS flight over people. The impact characteristics of any sUAS post in-flight failure must be known before operating over people to determine how much impact energy the vehicle may introduce during the collision. This paper focuses on Modeling and Simulation of sUAS post in-flight failure to estimate its impact characteristics. Quadrotor models of three commercial UAVs are developed. Their post failure trajectories are simul

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Jing, Chan Shi, Dwi Pebrianti, Goh Ming Qian, and Luhur Bayuaji. "Fault detection in quadrotor MAV." In 2017 7th IEEE International Conference on System Engineering and Technology (ICSET). IEEE, 2017. http://dx.doi.org/10.1109/icsengt.2017.8123422.

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