Publikační výsledky

• 2025

  ZIKMUND, P.; KOFLER, M.; NAVRÁTIL, J.; HRSTKA, M.; POLLÁK, J.; VAN KAMPEN, E. Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials. In 2024 New Trends in Aviation Development (NTAD). 2024 New Trends in Aviation Development (NTAD). IEEE, 2025. p. 236-241. ISBN: 979-8-3315-2774-7. ISSN: 2836-2764.
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• 2024

  ZIKMUND, P.; HORPATZKÁ, M.; PROCHÁZKOVÁ, H.; MACÍK, M. More Haptic Aircraft. In 13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons. Journal of Physics: Conference Series. IOP Publishing Ltd, 2024. no. 1, p. 1-8. ISSN: 1742-6596.
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  ZIKMUND, P.; HORPATZKÁ, M.; MACÍK, M. Learning effect in joystick tactile guidance. IEEE Transactions on Haptics, 2024, vol. 17, no. 4, p. 567-577. ISSN: 1939-1412.
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• 2020

  ZIKMUND, P.; DUBNICKÝ, L.; HORPATZKÁ, M.; MACÍK, M. Comparison of Joystick guidance methods. In 2019 10th IEEE International Conference on Cognitive Infocommunications (CogInfoCom). IEEE, 2020. p. 265-270. ISBN: 978-1-7281-4793-2.
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  ZIKMUND, P.; HORPATZKÁ, M.; DUBNICKÝ, L.; MACÍK, M.; JEBÁČEK, I. Pilot-aircraft haptic feedback tests. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2020, vol. 92, no. 9, p. 1407-1412. ISSN: 1748-8842.
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• 2019

  KOK, M., TOBIN, E. F., ZIKMUND, P., RAPS, D., YOUNG, T. Laboratory Investigation into Anti-contamination Coatings for Mitigating Insect Contamination with Application to Laminar Flow Technologies. In Contamination Mitigating Polymeric Coatings for Extreme Environments. Advances in Polymer Science. Springer International Publishing, 2019. p. 291-314. ISBN: 978-3-030-45839-3.
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  ZIKMUND, P.; DUBNICKÝ, L.; HORPATZKÁ, M.; MACÍK, M.; JEBÁČEK, I. Flight Test of Pilot-Aircraft Haptic Feedback System. In MATEC Web of Conferences. MATEC web of conferences. 9th EASN International Conference on “Innovation in Aviation & Space”. MATEC Web of Conferences, 2019. no. 304, p. 1-7. ISSN: 2261-236X.
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• 2018

  ZIKMUND, P.; MACÍK, M.; MÍKOVEC, Z. Reaction on directional vibrations applied on joystick. New Trends in Civil Aviation. London, UK: CRC Press, 2018. p. 107-111. ISBN: 978-0-8153-7602-6.
  Detail

  MALALAN, N.; ZIKMUND, P. Vibration Feedbacks in Pilot-Aircraft Haptic Interaction. In 13th Research and Education in Aircraft Design Conference. 2018. p. 98-108. ISBN: 978-80-214-5696-9.
  Detail

  ZIKMUND, P.; MACÍK, M.; DVOŘÁK, P.; MÍKOVEC, Z. Bio-inspired aircraft control. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2018, vol. 90, no. 6, p. 983-991. ISSN: 1748-8842.
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• 2017

  ZIKMUND, P.; MATĚJŮ, J. Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2017, vol. 231, no. 13, p. 2479-2486. ISSN: 0954-4100.
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• 2016

  MATĚJŮ, J.; ZIKMUND, P. WING TIP VORTEX RANS AND LES SIMULATION AND MEASUREMENT OF THE MEAN CHARACTERISTICS. In ENGINEERING MECHANICS 2016. Engineering Mechanics. 2016. p. 374-377. ISBN: 978-80-87012-59-8. ISSN: 1805-8248.
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• 2015

  ZIKMUND, P.; POPELA, R. Airliner-UAV Flight Formation in Climb Regime. World Academy of Science, Engineering and Technology, 2015, vol. 9, no. 10, p. 631-636. ISSN: 1307-6892.
  Detail

  ZIKMUND, P. Wake vortex gliding. Proceedings of 6th European Conference For Aeronautics And Space Sciences. Krakow, Poland: 2015. p. 1-8.
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• 2014

  ZIKMUND, P. Laboratory testing of insect contamination with application to laminar flow technologies, Part I: Variables affecting insect impact dynamics. Aerospace Science and Technology, 2014, vol. 2014, no. 39, p. 605-613. ISSN: 1270-9638.
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• 2013

  DVOŘÁK, P.; PEJCHAR, J.; ZIKMUND, P. Overview of Unmanned Aerial Systems Developed at the Institute of Aerospace Engineering. In New Trends in Civil Aviation 2013 conference proceedings. Brno: CERM, 2013. p. 16-21. ISBN: 978-80-7204-843-4.
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  ZIKMUND, P.; PEJCHAR, J. VUT 700 SPECTO project overview. In 5TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS). 2013. p. 1-8. ISBN: 978-84-941531-0-5.
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  ZIKMUND, P. Identifikace aerodynamických charakteristik atmosférického letadla z výsledků letových měření. VUT v Brně: VUT v Brně, 2013. 20 s.
  Detail

  ZIKMUND, P.; POPELA, R. Wake vortex gliding as a new propulsion concept for UAVs. Letecký zpravodaj, 2013, vol. 2013, no. 2, p. 14-16. ISSN: 1211-877X.
  Detail

  ZIKMUND, P. Identifikace aerodynamických charakteristik atmosférického letadla z výsledků letových měření. VUT v Brně, FSI, Letecký ústav: 2013.
  Detail

• 2010

  ZIKMUND, P. AERODYNAMIC CHARACTERISTICS IDENTIFICATION: METHODS OVERVIEW AND APPLICATION OF ERROR EQUATION METHOD. RESEARCH BULLETIN, 2010, vol. 2010, no. 1, p. 125-129. ISSN: 1425-2104.
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• 2009

  DRAHANSKÝ, M.; POPELA, R.; MARVAN, A.; ZIKMUND, P.; HOLENDA, S. SEDAQ - Ústředna pro sběr dat ze senzorů v UAV. Sborník příspěvků 9. mezinárodní vědecké konference MDS-PSL 2009. Brno: Univerzita Obrany, 2009. s. 28-31. ISBN: 978-80-7231-670-0.
  Detail

  ZIKMUND, P.; DOUPNÍK, P. Měřící systém pro identifikaci aerodynamických součinitelů na bezpilotním prostředku. In FSI Junior konference. Brno: VUT v Brně, 2009. s. 206-210. ISBN: 978-80-214-3834-7.
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• 2008

  ZIKMUND, P.; DOUPNÍK, P. VUT "SPECTO" Mini-UAV Aerodynamic Design. Letecký zpravodaj, 2008, vol. 2008, no. 2, p. 17-19. ISSN: 1211-877X.
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• 2007

  POPELA, R.; ZIKMUND, P.; VANĚK, F.; KOUŘIL, M. The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft. Letecký zpravodaj, 2007, vol. 2007, no. 3, p. 52-55. ISSN: 1211-877X.
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