Synonyms were used for: aircraft conference design lift
Search without synonyms: title: Vertical lift aircraft design conference

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    Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

    Turkmen, Abdullah / Altug, Erdinc | IEEE | 2020
    this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a ...

    Baseline Design of Propeller for an eVTOL Aircraft to Achieve Urban Air Mobility

    Faraaz, Mohammed / Faizan, Afreed / Badarinath, Mukunda et al. | IEEE | 2023
    . Multiple configurations such as coaxial tilt-rotor and hybrid lift + cruise were considered for the aircraft, and preliminary design calculations ...

    Anti-skid braking control system design for aircraft: Multi-phase schemes approach

    Lonbani, Mohammadali Aghakhani / Morandini, Marco / Astori, Paolo et al. | IEEE | 2017
    A multiphase approach is considered for the design of an aircraft anti-skid braking control system. A four-phase scheme, based on angular ...

    Modeling and Control Optimization of the Shaft Driven Lift Fan Engagement

    Jiang, Tianmu / Zhang, Xiaobo / Wang, Zhanxue | IEEE | 2023
    key component for short takeoff and vertical landing (STOVL) aircraft. Through lift fan engagement, the propulsion system can obtain high ...

    A Landing Dynamics Analysis Model For STOVL Aircraft

    Sivrioglu, Selim | IEEE | 2023
    This study focuses on the landing dynamics of a short takeoff and vertical landing (STOVL) aircraft from a modeling perspective. The ...

    Analytical model and control solutions for unmanned aerial vehicle maneuvers in a vertical plane

    Azimov, Dilmurat / Allen, John | IEEE | 2017
    In this study, we present a class of nonlinear analytical solutions for the dynamics of a fixed wing unmanned aircraft vehicle (UAV). These ...

    Trajectory computation Infrastructure based on BADA Aircraft Performance Model

    Gallo, Eduardo / Lopez-Leones, Javier / Vilaplana, Miguel A. et al. | IEEE | 2007
    the “aircraft intent” (AI). Three of them set the position of the landing gear, high lift devices, and speed brakes, while the ...

    Research on Structural and Aeroelastic Design of a Hybrid Multi-rotor UAV

    Yang, Chuanguang / Ma, Tielin / Zhang, Zilun et al. | IEEE | 2019
    The structural design of a Hybrid Multi-rotor UAV which is aimed to have both conventional take-off and landing (CTOL) and vertical take ...

    Attitude and velocity high-gain control of a tilt-trirotor UAV

    Canciello, Giacomo / Cavallo, Alberto / D'Amato, Egidio et al. | IEEE | 2017
    for fixed wing tilt rotors in view of the lift control during transition from hovering to forward flight. The nonlinear dynamics, the large ...

    On estimation of wind velocity, angle-of-attack and sideslip angle of small UAVs using standard sensors

    Johansen, Tor A. / Cristofaro, Andrea / Sorensen, Kim et al. | IEEE | 2015
    estimate and vertical accelerometer measurements, as would be expected since lift force can be modeled as a linear function of AOA in normal flight. ...

    Analysis of Advanced Flight Management Systems (FMS), Flight Management Computer (FMC) field observations trials: Area Navigation (RNAV) holding patterns

    Herndon, Albert A. / Cramer, Michael / Nicholson, Tommy et al. | IEEE | 2011
    anticipated that the resulting performance of the aircraft FMC will meet the procedure design requirements identified in the FAA criteria. The ...

    Analysis of advanced flight management systems (FMSS), flight management computer (FMC) field observations trials: Standard instrument departure with radius-to-fix (RF) path terminators

    Herndon, Albert / Cramer, Michael / Nicholson, Tommy et al. | IEEE | 2012
    of procedure design criteria and aircraft performance standards, the paths of various aircraft on the same procedure do not coincide and may ...

    Analysis of advanced flight management systems (FMSS), Flight management computer (FMC) field observations trials: Performance based navigation to X landing system (PBN to xLS)

    Herndon, Albert / Cramer, Michael / Miller, Sam et al. | IEEE | 2014
    current aircraft/avionics that might be used to fly them over a range of design and environmental conditions. The approach chosen for this ...