ANALYSIS OF FACTORS AFFECTING VARYING MAXIMUM RANGE ABILITY FOR UNMANNED AERIAL VEHICLE

Authors

  • Volodymyr Kharchenko National Aviation University Kosmonavta Komarova avenue 1, 03680, Kyiv, Ukraine
  • Ievgen Plakhotniuk National Aviation University Kosmonavta Komarova avenue 1, 03680, Kyiv, Ukraine

DOI:

https://doi.org/10.18372/2306-1472.54.3860

Keywords:

aeronautical range, alignment, balancing aircraft, glide, range, Unmanned Aerial Vehicle

Abstract

 We consider the importance of rejecting the controls for a particular unmanned aircraft in a hospital flight. It is shown how the balancing properties unmanned aircraft affect the flight range.

Author Biographies

Volodymyr Kharchenko, National Aviation University Kosmonavta Komarova avenue 1, 03680, Kyiv, Ukraine

Doctor of Engineering. Professor. Holder of a State Award in Science and Engineering of Ukraine. Winner of a State Prize of Ukraine in Science and Engineering.
Vice-Rector for Scientific-Research Work at the National Aviation University, Kyiv, Ukraine. Head of the Department of Air Navigation Systems, National Aviation University, Kyiv, Ukraine.
Education: Kyiv Civil Aviation Engineers Institute with a Degree in Radio Engineering, Kyiv, Ukraine (1967).
Research area: management of complex socio-technical systems, air navigation systems and automatic decision-making systems aimed at avoidance conflict situations, space information technology design, air navigation services in Ukraine provided by СNS/АТМ systems.
Publications: 400.

Ievgen Plakhotniuk, National Aviation University Kosmonavta Komarova avenue 1, 03680, Kyiv, Ukraine

Postgraduate student of the Department of Air Navigation Systems, National Aviation University, Kyiv, Ukraine.
Education: National Aviation University, Kyiv, Ukraine (2010).
Research area: unmanned aircraft.
Publications: 3.

References

Andreevsky, V.V.; Derkach, A.G. 1987. Definition of attainable aircraft on the trajectories of complex profile. Riga, RCAII. P. 6164 (in Russian). [Андреевскией В.В. Определение области достижимости самолета на траекториях сложного профиля / В.В. Андреевскией, А.Г. Деркач. – Рига: РКИИГА, 1987.  C. 6164.]

Lebedev, A.A.; Chernobrovkin, L.S. 1962. Flight dynamics of unmanned aerial vehicles. A manual for schools. Moscow, Oborongiz. 548 p. (in Russian) [Лебедев А.А. Динамика полета беспилотных летательных аппаратов: учебное пособие для вузов / А.А. Лебедев, Л.С. Чернобровкин.  Москва: Оборонгиз, 1962.  548 с.]

Skripnichenko, S.Yu. 1981. Fuel savings by reducing the loss of aerodynamic control for balancing. Questions GLA aerodynamics and strength. Moscow, State NIIGA. Issue 202: 5662 (in Russian). [Скрипниченко С.Ю. Экономия авиатоплива за счет снижения потерь аэродинамического качества на балансировку / С.Ю. Скрипниченко // Вопросы аэродинамики и прочности ГЛА. Москва: ГосНИИГА, 1981.  Выпуск 202. – С. 5662.]

Udartsev, E.P.; Pereverzev, A.M.; Ishchenko S.A. 1998. Operating aerodynamics. Trajectory problem. Manual. Kyiv, KMUGA. 136 p. (in Russian). [Ударцев Е.П. Эксплуатационная аэродинамика. Траекторные задачи: учебное пособие / Е.П. Ударцев, А.М. Переверзев, С.А. Ищенко. – Киев: КМУГА, 1998. – 136 с.]

Skripnichenko, S.Yu. 1988. Optimization of the flight based on economic criteria. Moscow, Mashinostroenie. 152 p. (in Russian). [Скрипниченко С.Ю. Оптимизация режимов полета по экономическим критериям / С.Ю. Скрипниченко. – Москва: Машиностроение, 1988. – 152 с.]

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How to Cite

Kharchenko, V., & Plakhotniuk, I. (2013). ANALYSIS OF FACTORS AFFECTING VARYING MAXIMUM RANGE ABILITY FOR UNMANNED AERIAL VEHICLE. Advances in Aerospace Technology, 54(1), 31–36. https://doi.org/10.18372/2306-1472.54.3860

Issue

Section

AEROSPACE SYSTEMS FOR MONITORING AND CONTROL

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