Advances in aircraft and spacecraft science

  • 제3권4호
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  • Pages.399-425
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  • 2016
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  • 2287-528X(pISSN)
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  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
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Airplanes at constant speeds on inclined circular trajectories

  • Labonte, Gilles (Department of Mathematics and Computer Science and Department of Electrical Engineering and Computer Engineering, Royal Military College of Canada)
  • 투고 : 2015.11.03
  • 심사 : 2015.12.27
  • 발행 : 2016.10.25
⟨ 이전 논문 다음 논문 ⟩

초록

The dynamical requirements are obtained for airplanes to travel on inclined circular trajectories. Formulas are provided for determining the load factor, the bank angle, the lift coefficient and the thrust or power required for the motion. The dynamical properties of the airplane are taken into account, for both, airplanes with internal combustion engines and propellers, and airplanes with jet engines. A procedure is presented for the construction of tables from which the flyability of trajectories at a given angle of inclination can be read, together with the corresponding minimum and maximum radii allowed. Sample calculations are shown for the Cessna 182, a Silver Fox like unmanned aerial vehicle, and a F-16 jet airplane.

키워드

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피인용 문헌

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  2. On determining the flyability of airplane rectilinear trajectories at constant velocity vol.5, pp.5, 2018, https://doi.org/10.12989/aas.2018.5.5.551
  3. Recent advances in unmanned aerial vehicles real-time trajectory planning vol.7, pp.4, 2016, https://doi.org/10.1139/juvs-2017-0004
  4. How airplanes fly at power-off and full-power on rectilinear trajectories vol.7, pp.1, 2016, https://doi.org/10.12989/aas.2020.7.1.053
  5. Point de référence pour la planification de trajectoires d’UAV à voilure fixe vol.9, pp.1, 2021, https://doi.org/10.1139/juvs-2019-0022
  6. Nonlinear Analysis and Bifurcation Characteristics of Whirl Flutter in Unmanned Aerial Systems vol.5, pp.4, 2016, https://doi.org/10.3390/drones5040122