Relevant bibliographies by topics / Rotary-wing UAV

Contents

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

Academic literature on the topic 'Rotary-wing UAV'

Author: Grafiati
Published: 4 June 2021
Last updated: 19 February 2022

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Journal articles on the topic "Rotary-wing UAV"

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Krishnakumar, R., K. Senthil Kumar, and T. Anand. "Design and Development of Vertical Takeoff and Horizontal Transition Mini Unmanned Aerial Vehicle." Advanced Materials Research 1016 (August 2014): 436–40. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.436.

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In recent years Unmanned Aerial Vehicles (UAV) has become a significant segment of the aviation industry. They can be chosen to be designed as fixed wing or Rotary wing type. Fixed-wing aircraft has the performance of fast forward movement, long range and superior endurance due to its gliding capabilities with no power. Unlike the fixed wing models, rotary wing mini-copters are able to fly in all directions, hover in a fixed position with minimal space for takeoff and landing. This makes them the perfect instrument for detailed inspection work or surveying. Implementing a hybrid UAV has the ad
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Peng, Kemao. "Autonomous Mission Management Based Nonlinear Flight Control Design for a Class of Hybrid Unmanned Aerial Vehicles." Guidance, Navigation and Control 01, no. 02 (June 2021): 2150009. http://dx.doi.org/10.1142/s2737480721500096.

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In this paper, a nonlinear flight control law is designed for a hybrid unmanned aerial vehicle (UAV) to achieve the advanced flight performances with the autonomous mission management (AMM). The hybrid UAV is capable of hovering like quadrotors and maneuvering as fixed-wing aircraft. The main idea is to design the flight control laws in modules. Those modules are organized online by the autonomous mission management. Such online organization will improve the UAV autonomy. One of the challenges is to execute the transition flight between the rotary-wing and fixed-wing modes. The resulting close
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ÜNAL, Beytullah, Tamer SAVAŞ, and Işıl YAZAR. "DESIGN OF A SPRAYING QUADCOPTER." First Issue of 2019, no. 2019.01 (December 18, 2019): 3–9. http://dx.doi.org/10.23890/ijast.2019.0101.

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Today, coupled with technological development, UAV (Unmanned Aero Vehicle) systems show an important improvement in civil area applications. UAV systems have active tasks with cost-effectively solutions in several areas like defense, logistics, engineering and agriculture. Especially, in agricultural applications, UAV system usage contributes to development of the critical parameters of this sector as efficiency and sustainability. Thus, in agricultural areas, improvement and usage of unmanned systems are of importance. In this study, a remote control rotary wing UAV system that has ability to
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Gonzalez, José Cerdeira, Roberto Ortiz Garrido, and Antonio Eduardo Carrilho da Cunha. "Rotary-Wing UAV Mission Planning Aided by Supervisory Control." IFAC Proceedings Volumes 43, no. 12 (2010): 324–30. http://dx.doi.org/10.3182/20100830-3-de-4013.00054.

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Zhan, Cheng, and Renjie Huang. "Energy Efficient Adaptive Video Streaming With Rotary-Wing UAV." IEEE Transactions on Vehicular Technology 69, no. 7 (July 2020): 8040–44. http://dx.doi.org/10.1109/tvt.2020.2993303.

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Ahmed, Bilal, Hemanshu R. Pota, and Matt Garratt. "Flight control of a rotary wing UAV using backstepping." International Journal of Robust and Nonlinear Control 20, no. 6 (May 12, 2009): 639–58. http://dx.doi.org/10.1002/rnc.1458.

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Zeng, Yong, Jie Xu, and Rui Zhang. "Energy Minimization for Wireless Communication With Rotary-Wing UAV." IEEE Transactions on Wireless Communications 18, no. 4 (April 2019): 2329–45. http://dx.doi.org/10.1109/twc.2019.2902559.

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Yan, Hua, Yunfei Chen, and Shuang-Hua Yang. "New Energy Consumption Model for Rotary-Wing UAV Propulsion." IEEE Wireless Communications Letters 10, no. 9 (September 2021): 2009–12. http://dx.doi.org/10.1109/lwc.2021.3090772.

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Guo, Huiqiang, Mingzhe Li, Pengfei Sun, Changfeng Zhao, Wenjie Zuo, and Xiaoying Li. "Lightweight and maintainable rotary-wing UAV frame from configurable design to detailed design." Advances in Mechanical Engineering 13, no. 7 (July 2021): 168781402110349. http://dx.doi.org/10.1177/16878140211034999.

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Rotary-wing unmanned aerial vehicles (UAVs) are widespread in both the military and civilian applications. However, there are still some problems for the UAV design such as the long design period, high manufacturing cost, and difficulty in maintenance. Therefore, this paper proposes a novel design method to obtain a lightweight and maintainable UAV frame from configurable design to detailed design. First, configurable design is implemented to determine the initial design domain of the UAV frame. Second, topology optimization method based on inertia relief theory is used to transform the initia
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Kumar, K. Senthil, and A. Mohamed Rasheed. "Development of Rotary Wing Mini UAS for Civilian Applications." Unmanned Systems 01, no. 02 (October 2013): 247–58. http://dx.doi.org/10.1142/s2301385013400050.

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This research paper is about team Dhaksha's accomplishment in designing, developing and testing a slew of Rotary Wing Mini Unmanned Aerial Systems for entry into various international aerial robotics/unmanned aerial vehicle (UAV) competitions and civilian applications. Dhaksha, the Unmanned Aircraft System (UAS), developed by the team at Madras Institute of Technology (MIT) campus of Anna University, Chennai, Tamil Nadu, India, with its stable design presented stiff competition to other contestants during the May 2012 technology demonstration called UAVForge organized by Defense Advanced Resea
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Dissertations / Theses on the topic "Rotary-wing UAV"

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Beyers, Coenraad Johannes. "Motion planning algorithms for autonomous navigation for a rotary-wing UAV." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/80231.

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Thesis (MScEng)--Stellenbosch University, 2013.<br>ENGLISH ABSTRACT: This project concerns motion planning for a rotary wing UAV, where vehicle controllers are already in place, and map data is readily available to a collision detection module. In broad terms, the goal of the motion planning algorithm is to provide a safe (i.e. obstacle free) flight path between an initial- and goal waypoint. This project looks at two specific motion planning algorithms, the Rapidly Exploring Random Tree (or RRT*), and the Probabilistic Roadmap Method (or PRM). The primary focus of this project is learni
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Kang, Keeryun. "Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles." Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/44820.

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This thesis presents an integrated framework for online obstacle avoidance of rotary-wing unmanned aerial vehicles (UAVs), which can provide UAVs an obstacle field navigation capability in a partially or completely unknown obstacle-rich environment. The framework is composed of a LIDAR interface, a local obstacle grid generation, a receding horizon (RH) trajectory optimizer, a global shortest path search algorithm, and a climb rate limit detection logic. The key feature of the framework is the use of an optimization-based trajectory generation in which the obstacle avoidance problem is formu
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McEwen, Matthew D. "Dynamic system identification and modeling of a rotary wing UAV for stability and control analysis." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA349878.

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Gleeson, Jeremy Information Technology &amp Electrical Engineering Australian Defence Force Academy UNSW. "Finding the shipboard relative position of a rotary wing unmanned aerial vehicle (UAV) with ultasonic ranging." Awarded by:University of New South Wales - Australian Defence Force Academy, 2008. http://handle.unsw.edu.au/1959.4/38978.

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Simple, cheap and reliable echo-based ultrasonic ranging systems such as the Polaroid ranging unit are easily applied to indoor applications. However, to measure the range between an unmanned helicopter and a moving ship deck at sea using ultrasound requires a more robust ranging system, because rushing air and breaking water are known ultrasound noise sources. The work of designing, constructing and testing such a system is described in this dissertation. The compact, UAV ready ultrasound transmitter module provides high power, broadband arbitrary signal generation. The separate field-ready r
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Rathore, Ankush, and ankushrathore@yahoo com. "A systems approach to model the conceptual design process of vertical take-off unmanned aerial vehicle." RMIT University. School of Aerospace, Mechanical and Manufacturing Engineering, 2006. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20061114.103443.

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The development and induction in-service of Unmanned Air Vehicles (UAV) systems in a variety of civil, paramilitary and military roles have proven valuable on high-risk missions. These UAVs based on fixed wing configuration concept have demonstrated their operational effectiveness in recent operations. New UAVs based on rotary wing configuration concept have received major attention worldwide, with major resources committed for its research and development. In this thesis, the design process of a rotary-wing aircraft was re-visualised from an unmanned perspective to address the r
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Ma, Ling. "Development of Fault Detection and Diagnosis Techniques with Applications to Fixed-wing and Rotary-wing UAVs." Thesis, 2011. http://spectrum.library.concordia.ca/7466/1/MA_MASc_S20..pdf.

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ABSTRACT Development of Fault Detection and Diagnosis Techniques with Applications to Fixed-wing and Rotary-wing UAVs Ling Ma Fault Detection and Diagnosis (FDD), as the central part of a Fault Tolerant Control System (FTCS), detects and diagnoses the source and the magnitude of a fault when a fault/failure occurs either in an actuator, sensor or in the system itself. This thesis work develops an applicable procedure for a FDD scheme to both fixed-wing and rotary-wing UAVs (Unmanned Aerial Vehicles) in the discrete-time stochastic domain based on the Kalman filter techniques. In particular,
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Books on the topic "Rotary-wing UAV"

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McEwen, Matthew D. Dynamic system identification and modeling of a rotary wing UAV for stability and control analysis. Monterey, Calif: Naval Postgraduate School, 1998.

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Dynamic System Identification and Modeling of a Rotary Wing UAV for Stability and Control Analysis. Storming Media, 1998.

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Book chapters on the topic "Rotary-wing UAV"

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Wu, Fahui, Dingcheng Yang, and Lin Xiao. "Energy Minimization for Rotary-Wing UAV Enabled WPCN." In Intelligent Robotics and Applications, 27–40. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-27538-9_3.

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Ahmed, Bilal, and Hemanshu R. Pota. "Dynamic Compensation for Control of a Rotary wing UAV Using Positive Position Feedback." In Unmanned Aerial Vehicles, 43–56. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-94-007-1110-5_5.

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Göktoğan, Ali Haydar, Salah Sukkarieh, Mitch Bryson, Jeremy Randle, Todd Lupton, and Calvin Hung. "A Rotary-wing Unmanned Air Vehicle for Aquatic Weed Surveillance and Management." In Selected papers from the 2nd International Symposium on UAVs, Reno, Nevada, U.S.A. June 8–10, 2009, 467–84. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-8764-5_24.

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Gomes, Alexandre, Bruno J. Guerreiro, Rita Cunha, Carlos Silvestre, and Paulo Oliveira. "Sensor-Based 3-D Pose Estimation and Control of Rotary-Wing UAVs Using a 2-D LiDAR." In ROBOT 2017: Third Iberian Robotics Conference, 718–29. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-70833-1_58.

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Conference papers on the topic "Rotary-wing UAV"

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Xu, Yaojin, Long Di, and YangQuan Chen. "Consensus Based Formation Control of Multiple Small Rotary-Wing UAVs." In ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/detc2011-47844.

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Small unmanned aerial vehicles (UAVs) can provide facilities in various applications. Compared with single UAV system, small UAVs based cooperative UAV system can bring advantages such as higher efficiency and safety. Therefore, it is necessary to design a robust multi-agent cooperative flight controller to coordinate a group of small UAVs for stable formation flights. This paper investigates the problem of consensus-based formation control for a multi-UAV system. Firstly, We choose a simplified model with nonholonomic constraints for UAV dynamics. Secondly, using the algebraic theory and back
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Bilal Ahmed, Hemanshu R. Pota, and Matt Garratt. "Rotary wing UAV position control using backstepping." In 2007 46th IEEE Conference on Decision and Control. IEEE, 2007. http://dx.doi.org/10.1109/cdc.2007.4434589.

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Hui Xie, Alan Lynch, and Martin Jagersand. "IBVS of a rotary wing UAV using line features." In 2014 IEEE 27th Canadian Conference on Electrical and Computer Engineering (CCECE). IEEE, 2014. http://dx.doi.org/10.1109/ccece.2014.6901119.

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Hanford, Scott, Lyle Long, and Joseph Horn. "A Small Semi-Autonomous Rotary-Wing Unmanned Air Vehicle (UAV)." In Infotech@Aerospace. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-7077.

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Ahmed, Bilal, Hemanshu R. Pota, and Matt Garratt. "Flight control of a rotary wing UAV - a practical approach." In 2008 47th IEEE Conference on Decision and Control. IEEE, 2008. http://dx.doi.org/10.1109/cdc.2008.4738917.

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Grobler, P. R., and H. W. Jordaan. "Autonomous Vision Based Landing Strategy for a Rotary Wing UAV." In 2020 International SAUPEC/RobMech/PRASA Conference. IEEE, 2020. http://dx.doi.org/10.1109/saupec/robmech/prasa48453.2020.9041238.

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Ahmed, Bilal, and Hemanshu R. Pota. "Flight control of a Rotary wing UAV using adaptive backstepping." In 2009 IEEE International Conference on Control and Automation (ICCA). IEEE, 2009. http://dx.doi.org/10.1109/icca.2009.5410398.

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Kong, Changduk, Jongha Park, and Myoungcheol Kang. "A Study on Transient Performance Characteristics of the CRW Type UAV Propulsion System During Flight Mode Transition." In ASME Turbo Expo 2005: Power for Land, Sea, and Air. ASMEDC, 2005. http://dx.doi.org/10.1115/gt2005-68400.

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A propulsion system of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) was composed of the turbojet engine, exhaust nozzles including some tip jet nozzles and a main nozzle and the duct system including straight ducts, curved ducts and master valve. The CRW type UAV has three different flight modes such as the rotary wing mode for take-off and landing, the high-speed forward flight mode with the fixed wing and the transition flight mode between the previously mentioned two flight modes. In order to evaluate transient performance characteristics of the CRW type UAV propulsion sys
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Wheeler, Jei. "Tactical Close Aerial Support for Public Events by Rotary Wing UAV." In Infotech@Aerospace. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-6953.

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Sanchez, L. A., O. Santos, H. Romero, S. Salazar, and R. Lozano. "Nonlinear and optimal real-time control of a rotary-wing UAV." In 2012 American Control Conference - ACC 2012. IEEE, 2012. http://dx.doi.org/10.1109/acc.2012.6315498.

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You might also be interested in the extended bibliographies on the topic 'Rotary-wing UAV' for particular source types:
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