Design and Implementation of A Low-Cost Parachute Landing System for Fixed-Wing Mini Unmanned Aerial Vehicles

Year 2024, Volume: 8 Issue: 3, 198 - 205

Fatma Yıldırım Dalkıran , Emre Kırteke

https://doi.org/10.30518/jav.1479457

Abstract

Fixed-wing mini-UAVs (Unmanned Aerial Vehicles) face difficulties due to the need for runways during take-off and landing. While fixed-wing UAVs are capable of using catapults during take-off, various landing systems are required for landing. Therefore, in this study, a parachute system design and production were carried out for the safe landing of fixed-wing mini-UAVs. The produced parachute utilized ultra-lightweight ripstop nylon fabric and suspension lines, while a carbon fiber tube was chosen for the launching system for its lightweight and strength. The parachute deployment system was triggered by a servo motor with low power consumption and high torque. During tests, the parachute was activated at a height of 47 meters during flight. The parachute deployment was completed in 1.42 seconds, and the descent with the parachute lasted 11 seconds. The vertical descent speed of the parachute during landing was measured at 4.27 m/s. The produced parachute landing system was manufactured at 71% lower cost compared to existing parachute landing systems in the literature and on the market. Additionally, the ultra-light ripstop parachute weighed 56 grams, making it 12% lighter than similar systems. Considering the advantages in terms of cost and weight, it is anticipated that parachute landing systems will be increasingly used for fixed-wing UAVs in the future.

Keywords

Fixed UAV, Parachute, Parachute Landing System, Parachute Fabric

Project Number

FYL-2022-12008

Thanks

This work has been supported by Erciyes University Scientific Research Projects Coordination. The unit is under grant number code FYL-2022-12008.

References

• Abinaya, R., Arravind, R. (2017). Selection of Low-Cost Recovery System for Unmanned Aerial Vehicle. International Research Journal of Engineering and Technology, 4(5), 1074-1078.
• Airbus. (2024). A 320 CEO Setting Single-Aisle Standards. https://aircraft.airbus.com/en/aircraft/a320-the- most-successful-aircraft-family-ever/a320ceo (Accessed on September 12, 2024).
• Al-Madani, B., Svirskis, M., Narvydas, G., Maskeliūnas, R. and Damaševičius, R. (2018). Design of Fully Automatic Drone Parachute System with Temperature Compensation Mechanism for Civilian and Military Applications. Journal of Advanced Transportation, 2018, ID 2964583, 1-11.
• Austin, R. (2010). Unmanned Aircraft Systems – UAVS Design, Development and Deployment. John Wiley &Sons Ltd. New Delhi, India.
• Bellis, M. (2019). History of the Parachute (Inventors and Innovations). https://www.thoughtco.com/history-of- the-parachute-1992334 (Accessed on April 20, 2024).
• Blom, J.D. (2010). Unmanned Aerial Systems: A Historical Perspective. Combat Studies Institute Press, US Army Combined Arms Center, Fort Leavenworth, Kansas.
• Copper, B. (2024). The Plane With A Parachute: A Guide To The Cirrus SR22. https://simpleflying.com/plane- with-parachute-cirrus-sr22-guide/ (Accessed on September 12, 2024).
• Federal Aviation Administration. (2015). Parachute Rigger Handbook, Oklahoma City, USA, pp. 1-350.
• Gleason, T.J. and Fahlstrom, P.G. (2016). Recovery of UAVs. Encyclopedia of Aerospace Engineering, John Wiley & Sons Ltd.
• Historical Review. (2024). https://www.parachutehistory. com/eng/drs.html (Accessed on April 20, 2024).
• Kekeç, E. T., Konar, M. and Yıldırım Dalkıran, F. (2020). Realization of Low Cost Useful Variometer Application for Sportive Aviation. Journal of Aviation, 4(1), 79-88.
• Kim, H.J., Kim, M., Lim, H., Park, C., Yoon, S., Lee, D., Choi, H., Oh, G., Park, J. and Kim, Y. (2013). Fully Autonomous Vision-Based Net-Recovery Landing System for a Fixed-Wing UAV. IEEE/ASME Transactions on Mechatronics, 18(4), 1320–1333.
• Knacke, T.W. (1991). Parachute Recovery Systems Design Manual. Para Publishing, Santa Barbara, California, USA.
• Mcwilliams, P. (2023). Different Parachute Types: Styles of Canopy for Skydiving. https://awe365.com/a- summary-of-different-parachute-types/ (Accessed on April 20, 2024).
• Oktay, T., Konar, M., Onay, M., Aydın, M. and Mohamed, M.A. (2016). Simultaneous Small UAV and Autopilot System Design. Aircraft Engineering and Aerospace Technology, 88, 818-834.
• Parachute. (2024). https://www.newworldencyclopedia.org/entry/Parachute (Accessed on April 20, 2024).
• Poynter, D. (1991). The Parachute Manual A Technical Treatise on Aerodynamic Decelerators. 4. Edition. Para Publishing, Santa Barbara, California, USA.
• Nakka, R. (2020). Parachute Design and Construction. https://www.nakka-rocketry.net/paracon.html (Accessed on May 5, 2024).
• Szafran, K.S. and Kramarski, I. (2019). Fatigue Degradation of the Ram-Air Parachute Canopy Structure. Fatigue of Aircraft Structures, 2019(11), 103–112.
• Ultimate Drone Parachute System for All Multicopters, Fixed Wing, UAS. (2024). https://fruitychutes.com/uav_rpv_drone_recovery_parachutes (Accessed on April 19, 2024).
• Williams, K.W. (2004). A Summary of Unmanned Aircraft Accident/Incident Data: Human Factors Implications. Federal Aviation Administration, Washington, DC, USA.
• Wilson, J. (2024). History of Parachuting and CSPA. https://www.cspa.ca/en/node/228 (Accessed on May 5, 2024).
• Wyllie, T. (2001). Parachute Recovery for UAV Systems. Aircraft Engineering and Aerospace Technology, 73(6), 542–551.
• Zakaria, M.Y. (2013). Design and Fabrication of Low-Cost Parachute Recovery System for SUAVs. 15th International Conference on Aerospace Sciences & Aviation Technology (ASAT – 15), May 28 - 30, 2013, Cairo, Egypt, 1-15.