Publications

• 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.
  Detail

  ZIKMUND, P.; HORPATZKÁ, M.; DUBNICKÝ, L.; MACÍK, M.; JEBÁČEK, I. Pilot-aircraft haptic feedback tests. Aircraft Engineering and Aerospace Technology - An International Journal, 2020, vol. 92, no. 9, p. 1407-1412. ISSN: 1748-8842.
  Detail | WWW | Full text in the Digital Library

• 2019

  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. p. 1-7. ISSN: 2261-236X.
  Detail | WWW | Full text in the Digital Library

  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.
  Detail | WWW

• 2018

  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 | WWW

  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 | WWW

  ZIKMUND, P.; MACÍK, M.; DVOŘÁK, P.; MÍKOVEC, Z. Bio-inspired aircraft control. Aircraft Engineering and Aerospace Technology - An International Journal, 2018, vol. 90, no. 6, p. 983-991. ISSN: 1748-8842.
  Detail | WWW

• 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.
  Detail | WWW | Full text in the Digital Library

• 2016

  MATĚJŮ, J.; ZIKMUND, P. WING TIP VORTEX RANS AND LES SIMULATION AND MEASUREMENT OF THE MEAN CHARACTERISTICS. In ENGINEERING MECHANICS 2016. Engineering mechanics 2014. 2016. p. 374-377. ISBN: 978-80-87012-59-8. ISSN: 1805-8248.
  Detail | WWW

  MATĚJŮ, J.; ZIKMUND, P. WING TIP VORTEX RANS AND LES SIMULATION AND MEASUREMENT OF THE MEAN CHARACTERISTICS. 2016. p. 374-377.
  Detail | WWW

• 2015

  ZIKMUND, P. Wake vortex gliding. Proceedings of 6th European Conference For Aeronautics And Space Sciences. Krakow, Poland: 2015. p. 1-8.
  Detail | Full text in the Digital Library

  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 | WWW

• 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.
  Detail | WWW

• 2013

  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.; 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

  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.
  Detail

  ZIKMUND, P. Identifikace aerodynamických charakteristik atmosférického letadla z výsledků letových měření. VUT v Brně: VUT v Brně, 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

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

  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. p. 28-31. ISBN: 978-80-7231-670-0.
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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.
  Detail

• 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.
  Detail

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