Abstract
UAV formation flight has many incomparable advantages with single UAV. In this paper, the “lead aircraft C wing aircraft” formation mode was used. The aerodynamic coupling effect of close formation, which was created by the leads vortex, was analyzed. Then the close formation equivalent aerodynamic model was established, which consists of two flying wing layout UAVs. The sliding mode variable structure control theory was introduced to design the UAV close formation controller. The controller was divided into longitudinal channel, lateral channel and vertical channel. These three channels were designed individually, thereby simplify the design of controller, reduce the parameters adjustment difficulty and explore a new method for close formation keeping research. The simulation results show that the formations geometry is maintained in the face of lead aircraft maneuver, and the feasibility and effectiveness of established UAV close formation flight controller was verified.
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References
Giulietti F, Innocenti M, Napolitano M (2005) Dynamic and control issues of formation flight. Aerosp Sci Technol 36(9):65–71
Zuo B, Hu Y (2004) UAV tight formation flight modeling and autopilot designing. In: Proceedings of the 5th world congress on intelligent control and automation. Hangzhou, China
SEMSAR E (2006) Adaptive formation control of UAVs in the presence of unknown vortex forces and leader commands. In: Proceedings of the 2006 American control conference min-neapolis. Minnesota, USA
Yong L, Micui W (2011) Close formation aerodynamic coupling effect analysis. Flight Dyn 19(2):12–16
Chundong C, Ruixuan W, Zhi D, Lipeng Z, Lei N (2012) Close formation coordinated flight control design for UAVs. Electron Opt Control 19(7):18–22
Chenggong L, Zhong Y, Qiongjian F (2009) Research on multi-UAVs close formation flight control based on CMAC. Transducer Microsyst Technol 28(7):37–40
ShengJun Q, Zhe Z (2012) Modeling and simulation of UAV close formation flight control. Adv Aeronaut Sci Eng 3(3):362–366
Pather M, Azzo JJ, Proud AW (2001) Tight formation flight control. J Guid Control Dyn 24(2):246–254
Andrew WP, Meir P, John JD (1999) Close formation flight control. AIAA, guidance, navigation, and control conference and exhibit
Jinkun L (2012) Sliding mode control design and matlab simulation. Tsinghua University Press, Beijing
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Li, Y., Zhou, G., Chen, W., Zhang, S. (2017). Design of UAV Close Formation Controller Based on Sliding Mode Variable Structure. In: Balas, V., Jain, L., Zhao, X. (eds) Information Technology and Intelligent Transportation Systems. Advances in Intelligent Systems and Computing, vol 454. Springer, Cham. https://doi.org/10.1007/978-3-319-38789-5_55
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DOI: https://doi.org/10.1007/978-3-319-38789-5_55
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