Showing 641 - 653 results of 653 for search '"fixed-wing"', query time: 0.07s Refine Results
  1. 641

    Preliminary Investigation of 4D Printing Technology for Deployable UAV Development by Chua, Chee Kai, Teoh, J. E. M., Liu, Yong, An, J., Li, Y.

    Published 2016
    “…Current unmanned aerial vehicles (UAVs) are large in size due to fixed wings and mechanical components. 4D printing is a technology that allows shape transformation (e.g. compaction, extension) of a 3D printed object. …”
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    Conference Paper
  2. 642

    A Review on the Current Status of Icing Physics and Mitigation in Aviation by Masafumi Yamazaki, Aleksandar Jemcov, Hirotaka Sakaue

    Published 2021-07-01
    “…The icing physics focuses on fixed wings, rotors, and engines severely impacted by icing. …”
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    Article
  3. 643

    Feasibility exploration of plasma actuation in flow control by Wong, Jun Jie.

    Published 2013
    “…They have been used in a wide range of applications that include bluff body wake control; lift augmentation and separation control on a variety of surfaces ranging from fixed wings with different degrees of sweep, wind turbine rotors and pitching airfoils simulating helicopter rotors, hypersonic flow separation, boundary layer flow control .New applications also include pollution control, semiconductor manufacturing, textile surface treatment, lightning arc drawings, lasers, plasma display panels, ozone generators etc.…”
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    Final Year Project (FYP)
  4. 644

    Accounting for aerodynamic Interference effects for a quadplane in transition flight by Shahriar, Fahim

    Published 2019
    “…Quadplane is a unique unmanned air vehicle (UAV) which has horizontal rotors and fixed wings. This prominent formation allows the vehicle to take off or land vertically, hover and transit to horizontal flight. …”
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    Thesis
  5. 645

    A Linear-Active-Disturbance-Rejection-Based Vertical Takeoff and Acceleration Strategy with Simplified Vehicle Operations for Electric Vertical Takeoff and Landing Vehicles by Shengchen Mao, Zheng Gong, Zheng Ye, Zian Wang, Tongqing Guo, Chengxi Zhang

    Published 2022-09-01
    “…Then, a simple vehicle operation method is defined for the vehicle, where the conventional operation method for fixed-wings and helicopters is considered for a friendly stick response definition for pilots with different backgrounds. …”
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    Article
  6. 646

    Conceptual Research on a Mono-Biplane Aerodynamics-Driven Morphing Aircraft by Tingyu Guo, Liangtao Feng, Chenhua Zhu, Xiaopeng Zhou, Haixin Chen

    Published 2022-07-01
    “…A new concept for a mono-biplane aerodynamics-driven morphing aircraft is proposed. The movable and fixed wings form a biplane mode during takeoff and landing, while they form a high aspect ratio monoplane mode when cruising. …”
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    Article
  7. 647

    Direct Entry Minimal Path UAV Loitering Path Planning by Jay P. Wilhelm, Garrett S. Clem, Gina M. Eberhart

    Published 2017-04-01
    “…Fixed Wing Unmanned Aerial Vehicles (UAVs) performing Intelligence, Surveillance and Reconnaissance (ISR) typically fly over Areas of Interest (AOIs) to collect sensor data of the ground from the air. …”
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    Article
  8. 648

    Training Sample Pattern Optimization Based on a Swarm Intelligence Algorithm for Tiltrotor Flight Dynamics Model Approximation by Jiayu Wen, Yanguo Song, Huanjin Wang, Dong Han, Changfa Yang

    Published 2023-11-01
    “…In the case of tiltrotor aircraft, the total number of aircraft states and controls is much greater than that of both traditional fixed-wings and helicopters. This requires, in general, a huge amount of training data for the network to reach a satisfactory approximation precision and makes the network size rise considerably. …”
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    Article
  9. 649

    The concept of vertical take-off and landing by using UAV mini model / Abdullah Syahril Mat Jani by Mat Jani, Abdullah Syahril

    Published 2004
    “…As we know, the VTOL airplane can be divided into two type of airplane. One is fix wing type that uses compressible engine to fly vertical and the other type is using blade to generate power to fly vertical (also known as rotary wing). …”
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    Thesis
  10. 650

    URANUS: Radio Frequency Tracking, Classification and Identification of Unmanned Aircraft Vehicles by Domenico Lofu, Pietro Di Gennaro, Pietro Tedeschi, Tommaso Di Noia, Eugenio Di Sciascio

    Published 2023-01-01
    “…We leverage real-time data provided by the Radio Frequency/Direction Finding system, and radars in order to detect, classify and identify drones (multi-copter and fixed-wings) invading no-drone zones. We adopt a Multilayer Perceptron neural network to identify and classify UAVs in real-time, with 90% accuracy. …”
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    Article
  11. 651

    Numerical Investigation on Intermittent Maximum Ice Accretion and Aerodynamic Performances of RG-15 Aerofoil at Low Reynolds Number by Haoyu Cheng, Dan Zhao, Nay Lin Oo, Xiran Liu, Xu Dong

    Published 2023-12-01
    “…Ice accretion is inevitable on fix-wing UAVs (unmanned aerial vehicles) when they are applied to surveillance and mapping over colder climates and arctic regions. …”
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    Article
  12. 652

    Evaluating the accuracy of unmanned aerial systems to quantify glacial ice habitats of harbor seals in Alaska by Courtney Pegus, Shannon Atkinson, Terry Quinn, Sanjay Pyare

    Published 2022-12-01
    “…Abstract Long‐term monitoring programs to evaluate climate‐driven changes to tidewater glaciers, an important habitat for harbor seals (Phoca vitulina) in Alaska, are primarily carried out by costly, weather‐dependent aerial surveys from fixed‐winged aircraft. Unmanned aerial systems (UAS) can be an alternative cost‐effective solution for gathering image data to quantify, monitor, and manage these habitats. …”
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    Article
  13. 653

    Evaluasi Metode Pengukuran Batimetri dan UAV untuk Mendukung Pembangunan Infrastruktur Pelabuhan Tanjung Adikarto by Faridatunnisa, Maritsa, Ulinnuha, Hilmiyati, Aji, Jongko Satrio, Azam, Kholqi, Basith, Abdul

    Published 2018
    “…Pengukuran batimetri dengan menggunakan dua peralatan single beam echosounder, pemetaan detil situasi dengan GPS geodetik metode RTK dan Total Stations, serta pemotretan UAV dengan wahana Fixed Wings. Hasil evaluasi dari ketiga metode ini adalah pelabuhan adikarto memiliki waktu-waktu tertentu untuk melakukan pengukuran batimetri area dangkal dan pengukuran metode RTK yaitu pada saat pagi dan sore hari. …”
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    Conference or Workshop Item