Global ETD Search

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Showing 1 to 5 of 5 for “"steady state flight"”.

  1. An experimental investigation on the distribution of the aerodynamic loads over the structural members of an inflatable, high aspect ratio (5.4), advanced concept paraglider

    … of an advanced concept para.glider at subsonic flight and low aerodynamic pressures, an experimental investigation was initiated and performed at the Langley Research Center. A paraglider model was designed and fabricated, and load recording balances were inserted within its structural members …

    vt Repository record for An experimental investigation on the distribution of the aerodynamic loads over the structural members of an inflatable, high aspect ratio (5.4), advanced concept paraglider (opens in a new tab)

  2. Modeling and Simulation of Vehicle Performance in a UAV Swarm Using Horizon Simulation Framework

    … and a pheromone map. Each vehicle operates at steady-state flight conditions of 36 m/s with an altitude of 1,800 m, and utilize an LQR set-point controller to maneuver through the pheromone map. All pheromone and aircraft related models are written in Python to expand the HSF scripting …

    calpoly Repository record for Modeling and Simulation of Vehicle Performance in a UAV Swarm Using Horizon Simulation Framework (opens in a new tab)

  3. The assessment of a rotorcraft simulation model in autorotation by means of flight testing a light gyroplane

    The simulation and flight testing of a light gyroplane aircraft is performed obtaining results regarding the flight dynamics attributes of the vehicle. The main aim of the work was to assess the ability of a mathematical model to simulate rotorcraft in the autorotative flight state. Additionally, …

    glasgow Repository record for The assessment of a rotorcraft simulation model in autorotation by means of flight testing a light gyroplane (opens in a new tab)

  4. A Simplified Icing Model for Simulation and Analysis of Dynamic Effects

    … aerodynamic surfaces are a major concern during flight. In this research effort, glaze ice is being modeled and its effects on aircraft dynamics analyzed. This type of ice builds up as a clear layer on aerodynamic surfaces and other components such as antennas and intakes. Glaze icing is …

    wvu Repository record for A Simplified Icing Model for Simulation and Analysis of Dynamic Effects (opens in a new tab)

  5. Dynamika letu a řízení

    Tato bakalářská práce se zabývá odvozením pohybových rovnic pro dynamickou soustavu letadla. Rovnice za předpokladu ustáleného přímočarého letu s malými odchylkami můžeme linearizovat a uplatnit teorii řízení. Výsledkem práce je vedle teoretické stránky také simulace pohybové odezvy na změnu polohy …

    brno-tech Repository record for Dynamika letu a řízení (opens in a new tab)