The Safe Auxiliary System for Aircraft’s Forced Landing

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Abstract:

Aiming at the abnormal landing of the aircraft which caused by the invalidation of the undercarriage, a safe auxiliary system for aircraft’s forced landing is proposed. Firstly, the article introduces the basic compositions and the main functions of each part in the system, and proposes the undercarriage robot based on the aircraft arresting system and also the underground rail system based on the steam-driven catapult principle is put forward. Secondly, the detail introductions on the system’s operating principles for aiding the forced landing of aircraft are given separately from starting, docking, decelerating and separation. At last, an expert control system based on knowledge base is proposed for realizing the calculation of docking position, velocity matching and the optimal decelerating scheme.

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306-310

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June 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] F J Momim, J R Arruda, D J Inman. Design of a reduced order H∞ controller for snlart structure satellite applications[J]. Phiosophical Transactions of the Royal Society: Mathematical, Physical and Engineering Sciences, 2001, 359: 2251- 2269.

DOI: 10.1098/rsta.2001.0885

Google Scholar

[2] Meng Wenjie, Li Aijun, ect, Design and simulation of controller of elasticity aircraft [J]. Computer Simulation, 2010, 27(12): 65-69.

Google Scholar

[3] Brahney, J H Mobile, Arresting system now being deployed [J], Aerospace Engineering, 1986(6): 22-26.

Google Scholar

[4] Flu Y M, Hu Z X. An approximately way of the nonlinear system[J], Control theory and application, 2001, 18(2): 160-165.

Google Scholar

[5] Zhang Li, The preliminary scheme to solve the problem of aircraft's not landing for the reason of undercarriage's problem[J], Journal of Civil Aviation Flight University of China, 2008, 19(9): 22- 24.

Google Scholar

[6] Soft-Ground Aircraft Arresting System for commercial Aircraft, Interimrept. AD-A263461, (1993).

Google Scholar

[7] Koichi Suyama. Reliable Nonlinear Control Systems[J], Electronics and Communications in Japan, 1999, 82(1): 953-962.

Google Scholar