A Method of Height Adjustment for Unpowered Emergency Landing

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The aircraft needs to adjust its heading angle to go to the landing window after the loss of thrust. However, the actual height of the aircraft within the landing area may be higher than that of the landing window. In order to ensure a safe landing, a spiral drop is needed to lose height. Through some certain integer rings of spiral, the aircraft will fall into the landing window. On this stage of height loss, this paper proposes a method of height adjustment to make the aircraft land exactly into the window. This method can get the desired bank angle through calculating the height difference between the height in the landing area, where the aircraft is, and the height of the landing window. This bank angle ensures the aircraft just to go through exactly the landing window in integer spiral rings of falls. Finally through simulation, this paper tests the effectiveness of the method.

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1410-1415

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October 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Dubins, L.E., On curves of minimal length with a constraint on average curvature, and with prescribed initial and terminal positions and tangents. American Journal of mathematics, 1957. 79(3): pp.497-516.

DOI: 10.2307/2372560

Google Scholar

[2] Hota, S. and D. Ghose. Optimal geometrical path in 3D with curvature constraint. in Intelligent Robots and Systems (IROS), 2010 IEEE/RSJ International Conference on. 2010. IEEE.

DOI: 10.1109/iros.2010.5653663

Google Scholar

[3] Blasi, L., S. Barbato, and M. Mattei, A particle swarm approach for flight path optimization in a constrained environment. Aerospace Science and Technology, 2013. 26(1): pp.128-137.

DOI: 10.1016/j.ast.2012.02.021

Google Scholar

[4] Shanmugavel, M., A. Tsourdos, B. White, and R. Żbikowski, Co-operative path planning of multiple UAVs using Dubins paths with clothoid arcs. Control Engineering Practice, 2010. 18(9): pp.1084-1092.

DOI: 10.1016/j.conengprac.2009.02.010

Google Scholar

[5] Ambrosino, G., M. Ariola, U. Ciniglio, F. Corraro, E. De Lellis, and A. Pironti, Path generation and tracking in 3-D for UAVs. Control Systems Technology, IEEE Transactions on, 2009. 17(4): pp.980-988.

DOI: 10.1109/tcst.2009.2014359

Google Scholar

[6] Heejun, C. and A. Ella, Smooth Transitions for a Turning Dubins Vehicle, in AIAA Guidance, Navigation, and Control Conference. 2010, American Institute of Aeronautics and Astronautics.

DOI: 10.2514/6.2010-7551

Google Scholar