Abstract
In the paper, influence of UAV control system redundancy and constrains on control system reconfiguration performances are investigated. A nonlinear model of a UAV aircraft with decoupled control surfaces is presented. A nonlinear model-based control allocation method is established for control system reconfiguration in the event of control surface jam. The aim of presented reconfiguration method is to obtain controllability performances of a damaged aircraft as close as possible to an undamaged one. The UAV aircraft model has been used to assess and demonstrate the proposed control system reconfiguration algorithms performances resulting from control system redundancy and constrains. The test results analysis, conclusions and recommendations for the aircraft reconfigurability improvement are presented as well.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Bodson M (2003) Reconfigurable nonlinear autopilot. J Guid Control Dyn 26(5):719–727
Burcham B (1997) Landing safely when flight controls fail. Aerosp Am 35(10):20–23
Fekri S, Gu D, Postlethwaite I (2009) Lateral imbalance detection on a UAV based on multiple models. In: Joint 48th IEEE conference on decision and control and 28th Chinese control conference, pp 8488–8493. Shanghai, 16–18 Dec 2009
Hass RA, Wells, SR (2003) Sliding mode control applied to reconfigurable flight control design. J Guid Control Dyn 26(3):452–461
Kozak V, Shevchuk D, Kravchuk N, Vasilyev M (2013) Intelligent active fault tolerant control system and flight safety. In: Th 7-th IEEE international conference on intelligent data acquisition and advanced computing systems: technology and application, pp 912–916. Berlin, 12–14 Sept 2013
Kozak V, Shevchuk D, Vovk V, Levchenko M (2014) Automation of aircraft control Rreconfiguration in flight special situations. In: Proceedings of IEEE 3rd international conference on methods and systems of navigation and motion control, pp 14–17. Kyiv (2014)
Lin X, Fulton NL, Horn MET (2014) Quantification of high level safety criteria for civil unmanned aircraft systems. In: Proceedings of aerospace conference, big sky, pp 1–13
Loh R, Bian Y, Roe T (2009) UAVs in civil airspace: safety requirements. IEEE Aerosp Electron Syst Maga 24(January):5–17
Lyu Y, Pan Q, Zhao C, Zhang Y, Hu J (2016) Vision-based UAV collision avoidance with 2D dynamic safety envelope. IEEE Aerosp Electron Syst Mag 31(7):16–26
Masui K, Tomita H, Komatsu Y (2004) Flight experiment on flight path optimization algorithm for aircraft in trouble. In: Proceedings of 24th international conference of the aeronautical science
Naskar A, Patra S, Sen S (2015) Reconfigurable direct allocation for multiple actuator failures. IEEE Trans Control Syst Technol 23(1):397–405
Nussberger A, Grabner H, Van Gool L (2016) Robust aerial object tracking from an airborne platform. IEEE Aerosp Electron Syst Mag 31(7):38–46
Peni T, Vanek B, Szabo Z, Bokor J (2014) Supervisory fault tolerant control of the NASA AirStar aircraft. Am Control Conf Portland 4–6(June):666–671
Steinberg M (2005) A historical overview of research in reconfigurable flight control. Proc Inst Mech Eng Part G: J Aerosp Eng 219:263–275
Suzuki S, Kawamura F, Masui K (2004) Autonomous flight control and guidance system of accident aircraft. In: Proceedings of 24th international conference of the aeronautical science
Yang Z, Hua S, Hongzhuan Q, Chengrui L (2012) Control reconfigurability of nonlinear system based on control redundancy. In: 10th IEEE international conference on industrial informatics (INDIN), pp 815–820. Beijing
Zhang Y, Jiang J (2003) Bibliographical review on reconfigurable fault tolerant control systems. In: 5th IFAC symposium on fault detection, supervision and safety for technical processes. Washington, D.C
\(\dot{Z}\)ugaj M, Bibik P, Jacewicz M (2016) UAV aircraft model for control system failures analysis. J Theor Appl Mech 54(4): 1405–14015
\(\dot{Z}\)ugaj M, Narkiewicz J (2009) Autopilot for reconfigurable flight control system. ASCE J Aerosp Eng 22(1): 78–84
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2018 Springer International Publishing AG
About this paper
Cite this paper
Żugaj, M. (2018). UAV Control System Reconfiguration Under Physical Constrains. In: Dołęga, B., Głębocki, R., Kordos, D., Żugaj, M. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Cham. https://doi.org/10.1007/978-3-319-65283-2_13
Download citation
DOI: https://doi.org/10.1007/978-3-319-65283-2_13
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-65282-5
Online ISBN: 978-3-319-65283-2
eBook Packages: EngineeringEngineering (R0)