Publications

• 2024

  BALÁŽOVÁ, R.; HLINKA, J.; BELBACHIR, A.; SVOBODA, J. Hyperlocal Weather Information for Drone Operations. In PROCEEDINGS OF THE 24TH INTERNATIONAL CONFERENCE ON NEW TRENDS IN CIVIL AVIATION 2024. New Trends in Civil Aviation (NTCA). 1. PRAGUE, CZECH REPUBLIC: Czech Technical University in Prague, 2024. p. 67-73. ISBN: 978-80-01-07182-3. ISSN: 2694-7854.
  Detail | WWW

  BALÁŽOVÁ, R.; HLINKA, J.; FERRARI, S.; SANTUS, A. Turbulence estimation by eddy dissipation rate at low-altitudes using UAV in-situ data. In ENGINEERING MECHANICS 2024 30th INTERNATIONAL CONFERENCE. Engineering Mechanics .... 1. Brno: Brno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, 2024. p. 42-45. ISBN: 978-80-214-6235-9. ISSN: 1805-8248.
  Detail | WWW | Full text in the Digital Library

• 2023

  HORPATZKÁ, M.; HLINKA, J. SUMMARY OF PERSPECTIVES IN ACTIVE SIDESTICKS DEVELOPMENT FOR SMALL AIRCRAFT FLY-BY-WIRE SYSTEMS. ENGINEERING MECHANICS 2023. Praha: Institute of Thermomechanics of the Czech Academy of Sciences, 2023. p. 91-94. ISBN: 978-80-87012-84-0.
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  VALIŠ, D.; HLINKA, J.; KOLÁČEK, J.; PROCHÁZKA, P.; CIPÍN, R.; POKORA, O.; KOŠTIAL, R. Comprehensive study on reliability, deterioration, and ageing of lithium-ion batteries in electric-powered aircraft assessed after a storage period using functional data analysis and non-parametric back up. ENGINEERING FAILURE ANALYSIS, 2023, vol. 154, no. 1, p. 1-27. ISSN: 1873-1961.
  Detail | WWW

• 2021

  HLINKA, J.; KOŠTIAL, R.; HORPATZKÁ, M. Application of enhanced methods for safety assessment of FADEC. EKSPLOAT NIEZAWODN, 2021, vol. 23, no. 1, p. 63-73. ISSN: 1507-2711.
  Detail | WWW | Full text in the Digital Library

• 2020

  JURAČKA, J.; HLINKA, J. Verified set of models for performance improvements based on analysis of existing operational data. Letecký ústav, VUT-FSI v Brně: 2020. p. 1-52.
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  HADAŠ, Z.; HLINKA, J.; JANÁK, L.; KŠICA, F.; RUBEŠ, O.; ŠEVEČEK, O.; TOFEL, P. Energy Harvesting Technologies for Structural Health Monitoring of Airplane Components-A Review. SENSORS, 2020, vol. 20, no. 22, p. 1-57. ISSN: 1424-8220.
  Detail | WWW

• 2019

  KŠICA, F.; HADAŠ, Z.; HLINKA, J. Integration and test of piezocomposite sensors for structure health monitoring in aerospace. MEASUREMENT, Journal of the International Measurement Confederation (IMEKO), 2019, vol. 147, no. 106861, p. 1-10. ISSN: 0263-2241.
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• 2018

  ŠPLÍCHAL, J.; HLINKA, J. MODELLING OF HEALTH MONITORING SIGNALS AND DETECTION AREAS FOR AEROSPACE STRUCTURES. In RESEARCH AND EDUCATION IN AIRCRAFT DESIGN (READ 2018). 2018. p. 170-188. ISBN: 978-80-214-5696-9.
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  JANHUBA, L.; HLINKA, J.; KOŠTIAL, R. Integrated Method utilizing Graph Theory and Fuzzy Logic for Safety and Reliability Assessment of Airborne Systems. In 13th Research and Education in Aircraft Design Conference. 2018. p. 32-44. ISBN: 978-80-214-5696-9.
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  KŠICA, F.; HADAŠ, Z.; HLINKA, J. Application of piezoelectric sensors for structural health monitoring in aerospace. In 2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Proceedings. Rome, Italy: Institute of Electrical and Electronics Engineers Inc., 2018. p. 596-601. ISBN: 978-1-5386-2473-9.
  Detail | WWW

  KOŠTIAL, R.; JANHUBA, L.; HLINKA, J. AIRCRAFT LEADING EDGES MINOR DAMAGES DETECTION BASED ON THERMOGRAPHIC SURVEY OF ELECTRICAL ANTI-ICING SYSTEM. In 13th Research and Education in Aircraft Design Conference. 2018. p. 15-22. ISBN: 978-80-214-5696-9.
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• 2017

  KOŠTIAL, R.; JANHUBA, L.; HLINKA, J. INTELLIGENT SCHEDULED MAINTENANCE METHODOLOGY FOR GENERAL AVIATION STRUCTURES BASED ON MSG-3 AND MULTIPLE- CRITERIA DECISION MAKING ANALYSIS. In Engineering Mechanics 2017. Engineering mechanics 2014. 1. Praha: ACAD SCI CZECH REPUBLIC, INST THERMOMECHANICS, DOLEJSKOVA 5, PRAGUE 8, 182 00, CZECH REPUBLIC, 2017. p. 498-501. ISBN: 978-80-214-5497-2. ISSN: 1805-8248.
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• 2015

  ŠPLÍCHAL, J.; PÍŠTĚK, A.; HLINKA, J. Dynamic tests of composite panels of an aircraft wing. PROGRESS IN AEROSPACE SCIENCES, 2015, vol. 2015, no. 78, p. 50-61. ISSN: 0376- 0421.
  Detail | WWW

• 2014

  SYMONOV, V.; POPELA, R.; HLINKA, J.; JEBACEK, I. Composite Wing Leading Edge Design: Technical Specification. 2014. p. 1-13.
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  HLINKA, J.; TREFILOVÁ, H. Identification of Major Safety Issues for Futuristic Personal Plane Concept. AVIATION, 2014, vol. 2014, no. 18(3), p. 120-128. ISSN: 1648-7788.
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• 2012

  HLINKA, J. Zamíří osobní doprava do vzduchu?. Praha: MAFRA, a.s. (Lidové noviny), 2012. p. 20-20.
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  ČERVINKA, D.; KLÍMA, B.; PAZDERA, I.; PÍŠTĚK, A.; HLINKA, J. Battery System of Electric Airplane VUT 051 RAY. ECS Transaction, 2012, vol. 2012, no. 40, p. 267-273. ISSN: 1938- 6737.
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• 2010

  HLINKA, J.; ŠPLÍCHAL, M.; MATĚJÁK, V. SECURITY REQUIREMENTS AND PLAN FOR SELECTED CZECH AIRPORT. Brno: 2010. p. 1-48.
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  HLINKA, J.; TREFILOVÁ, H. Safety and Security Aspects of the PPlane. VUT- FSI v Brně: 2010.
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  HLINKA, J.; ŠPLÍCHAL, M. Brno University of Technology: Space Activities of Research Establishments and Academia in Czech Republic. Transfer, 2010, vol. 2010, no. 13, p. 39-46. ISSN: 1801- 9315.
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• 2009

  PÍŠTĚK, A.; HLINKA, J.; URÍK, T.; ŠPLÍCHAL, M. VUT 001 MARABU: Design philosophy and realization of an experimental aircraft supporting UAV applications in civil sector. In Unmanned Air Vehicle Systems. Bristol, UK: University of Bristol, 2009. p. 37.1-37.11. ISBN: 978-0-9552644-5-0.
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  HLINKA, J. Modelování spolehlivosti a bezpečnosti systému jako celku. In Analýzy spolehlivosti a bezpečnosti v praxi (aneb jak přesvědčit zákazníka, že požadavky na spolehlivost a bezpečnost výrobku budou splněny). Novotného lávka 5, 116 69 Praha 1: Česká společnost pro jakost, 2009. p. 51-65. ISBN: 978-80-02-02156- 8.
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• 2008

  FINDA, J.; HLINKA, J.; WEISMAN, A. Relation Between Safety Assessment Methods and Reliability Centered Maintenance- Impact on the Aircraft Systems Architecture. Letecký zpravodaj, 2008, vol. 2008, no. 2, p. 9-15. ISSN: 1211- 877X.
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  HLINKA, J.; WEISMAN, A. Experience with Failure Rate Estimates and Component Importance Measures for General Aviation Aircraft Systems. In Reliability, Safety and Diagnostics of Transport Structures and Means. 1. Pardubice: University of Pardubice, 2008. p. 95-103. ISBN: 978-80-7395-096- 5.
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  PÍŠTĚK, A.; HLINKA, J. Development and Realization of VUT 001 MARABU Aircraft for Experimental Verification of UAV Systems. Sborník 1. Národní konference Civilní bezpilotní systémy. Ústav letadlové techniky, ČVUT v Praze, FS, Karlovo Náměstí 13, 121 35 Praha 2: Česká odborná společnost letecká, 2008. ISBN: 978-80-902522-2- 6.
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• 2007

  HLINKA, J. Safety/ Reliability Analyses of GA Aircraft in Design and Certification Stage in Czech Republic. AVIATION, 2007, vol. XI, no. 4, p. 14-23. ISSN: 1648- 7788.
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  HLINKA, J. Comparison of Reliability Analyses in Design Stage for Aviation and Space Applications. Acta Avionica, 2007, vol. IX, no. 13, p. 1-9. ISSN: 1335- 9479.
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  HLINKA, J.; PÍŠTĚK, A. EDUCATION, PROJECTS AND OTHER AEROSPACE ACTIVITIES ON BRNO UNIVERSITY OF TECHNOLOGY (CZECH REP.). In 1st CEAS European Air and Space Conference. Druckerei Thierbach, Elbestrasse 32, D-45478 Mulheim/ Ruhr: Deutsche Gesellschaft fur Luft und Raumfahrt (DGLR) - Godesberger Alle 70, D- 53175 Bonn, 2007. p. 1121-1126. ISBN: 3-938738-09- X.
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  HLINKA, J.; FINDA, J. Reliasoft BlockSim a zkušenosti s jeho využitím k analýzám bezporuchovosti letadlových soustav. 2006. Česká společnost pro jakost, 27. setkání odborné skupiny pro spolehlivost (Novotného lávka 5, 116 68 Praha 1): Česká společnost pro jakost, 2007. p. 48-57.
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• 2006

  PÍŠTĚK, A.; HLINKA, J. Aerospace Research in the Czech Republic and Cooperation with Europe. 2006. Aeronautics Days 2006, 19.-21.6.2006, Vídeň, Rakousko: 2006.
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  NOVÁK, J.; HLINKA, J. Spolehlivostní analýza a zkoušky části letadlové hydraulické soustavy. In Proceedings of the 19thInternational Conference on Hydraulics and Pneumatics. 1. Ostrava: Česká strojnická společnost, 2006. p. 106-114. ISBN: 80-02-01809- 5.
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  PÍŠTĚK, A.; HLINKA, J. Aerospace Research at Brno University of Technology - Czech Rep. and Cooperation with European Universities and Institutions. 2006. Conference on Cooperation with European Universities and Institutions, May 2006, Berlin, Německo: 2006.
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  HLINKA, J. Analýza způsobů a důsledků poruch (FMEA) mechanické části mikroakcelerometru MAC- 04. LÚ 51/ 2006. Letecký ústav, VUT- FSI v Brně: LÚ, 2006. p. 1-82.
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  HLINKA, J. Analýza způsobů a důsledků poruch (FMEA) mechanismu aretace mikroakcelerometru MAC- 04. LÚ 52/ 2006. Letecký ústav, VUT- FSI v Brně: 2006. p. 1-50.
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• 2005

  HLINKA, J.; NOVÁK, J. Reliability Analysis of Small Sport Airplane. In Reliability, Safety and Diagnostics of Transport Structures and Means 2005. Pardubice, Czech Republic: University of Pardubice, 2005. p. 119 ( p.)ISBN: 80-7194-769- 5.
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  HLINKA, J.; MŽIK, T. Reliability of Aircraft in Design and Certification Stage. In Reliability, Safety and Diagnostics of Transport Structures and Means 2005. Pardubice, Czech Republic: University of Pardubice, 2005. p. 239 ( p.)ISBN: 80-7194-769- 5.
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  HLINKA, J. SAFETY ANALYSES OF AIRCRAFT AVIONIC SYSTEMS (on the aircraft level). Letecký zpravodaj, 2005, vol. 2005, no. 3, p. 31-33. ISSN: 1211- 877X.
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• 2004

  HLINKA, J. APPLICATION OF DEPENDABILITY ANALYSIS DURING CERTIFICATION OF AIRPLANES. In Advanced Engineering Desing. University of Glasgow, UK: 2004. p. 1 ( p.)ISBN: 80-86059-39- 1.
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  HLINKA, J. POŽADAVKY PŘEDPISŮ A APLIKACE ANALÝZ SPOLEHLIVOSTI BĚHEM VÝVOJE A CERTIFIKACE MALÝCH LETADEL. In Opotřebení, spolehlivost, diagnostika 2004. Vojenská akademie v Brně: 2004. p. 1 ( p.)ISBN: 80-85960-77- X.
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  HLINKA, J. Application of Reliability Analysis During Certification of GA Airplanes. Letecký zpravodaj, 2004, vol. 2004, no. 3, p. 19 ( p.)ISSN: 1211- 877X.
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• 2003

  VANĚK, F.; HLINKA, J. Glauert III. 2003.
  

  HLINKA, J. Metodika detekce trhlin metodou vířivých proudů. 2003.
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  HLINKA, J. Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification. Letecký zpravodaj, 2003, vol. 2003, no. 3, p. 48 ( p.)ISSN: 1211- 877X.
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  HLINKA, J. RELIABILITY OF GENERAL AVIATION CLASS AIRCRAFT MECHANICAL SYSTEMS. In 3rd International Conference on Advanced Engineering Design. ČVUT, Praha: 2003. p. 1 ( p.)ISBN: 80-86059-35- 9.
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• 2002

  HLINKA, J. Požadavky na spolehlivost letounů obsažené v předpisech FAR část 23 a část 25. Letecký zpravodaj, 2002, vol. 2002, no. 4, p. 22 ( p.)ISSN: 1211- 877X.
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