Abstract
This paper proposes a decoupling control strategy for aircraft with thrust vector at high angle of attack. To eliminate strong couplings among different channels, the three-channels controllers are designed independently, respectively. The channels coupling, aerodynamic uncertainties, unmodeled dynamics, and external disturbance are regarded as generalized disturbance and extended into a new state, which is estimated and compensated in real time by extended state observer (ESO). The sliding mode control (SMC) method is employed to achieve the expected control performance. The numerical simulations demonstrate the effectiveness of the proposed control strategy.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Wu DW, Chen M, Gong HJ (2017) Robust control of post-stall pitching maneuver based on finite-time observer. ISA Trans 70(4):53–63. https://doi.org/10.1016/j.isatra.2017.06.015
Yang JL, Zhu JH (2016) A hybrid NDI control method for the high-alpha super-maneuver flight control. In: Proceedings of American Control Conference, Boston, MA, USA, pp 6747–6753. IEEE. https://doi.org/10.1109/ACC.2016.7526734
Mukherjee BK, Thomas P, Sinha M (2016) Automatic recovery of a combat aircraft from a completed cobra and herbst maneuver: a sliding mode control based scheme. In: Proceedings of Indian Control Conference, Hyderabad, India, pp 44–46. IEEE. https://doi.org/10.1109/INDIANCC.2016.7441137
Sinha M, Kuttieri R, Ghosh A, Misra A (2013) High angle of attack parameter estimation of cascaded fins using neural network. J Guidance Control Dyn 50(1):272–291. https://doi.org/10.2514/1.C031912
Snell S, Enns D, Garrard W (1992) Nonlinear inversion flight control for a supermaneuverable aircraft. J Guidance Control Dyn 15(4):976–984. https://doi.org/10.2514/3.20932
Adams R, Buffington J, Banda S (1994) Design of nonlinear control laws for high-angle-of-attack flight. J Guidance Control Dyn 17(4):737–746. https://doi.org/10.2514/3.21262
Seshagiri S, Promtun E (2008) Sliding mode control of F-16 longitudinal dynamics. In: Proceedings of American Control Conference, Seattle, Washington, USA, pp 1520-1532. IEEE. https://doi.org/10.1109/ACC.2008.4586748
Chiang R, Safonov M, Haiges K (1993) A fixed \(H_\infty \) controller for a supermaneuverable fighter performing the herbst maneuver. Automatica 29(1):111–127. https://doi.org/10.1016/0005-1098(93)90176-T
Han JQ (2009) From PID to active disturbance rejection control. IEEE Trans Ind Electron 56(3):900–906. https://doi.org/10.1109/TIE.2008.2011621
Gao ZQ (2014) On the centrality of disturbance rejection in automatic control. ISA Trans 53(4):850–857. https://doi.org/10.1016/j.isatra.2013.09.012
Sonneveldt L (2010) Nonlinear F-16 model description. Technical report, Delft University of Technology, The Netherlands
Han JQ (2008) Active disturbance rejection control technique-the technique for estimating and compensating the uncertainties. National Defense Industry Press, Beijing
Zheng Q, Dong LL, Lee D, Gao ZQ (2009) Active disturbance rejection control for MEMS gyroscopes. IEEE Trans Control Syst Technol 17(6):1432–1438. https://doi.org/10.1016/0005-1098(93)90176-T
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Liu, J., Chen, Z., Sun, M., Sun, Q. (2020). High Angle of Attack Sliding Mode Control for Aircraft with Thrust Vector Based on ESO. In: Jia, Y., Du, J., Zhang, W. (eds) Proceedings of 2019 Chinese Intelligent Systems Conference. CISC 2019. Lecture Notes in Electrical Engineering, vol 592. Springer, Singapore. https://doi.org/10.1007/978-981-32-9682-4_6
Download citation
DOI: https://doi.org/10.1007/978-981-32-9682-4_6
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-32-9681-7
Online ISBN: 978-981-32-9682-4
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)