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Design and Co-simulation of an Antiskid Brake System for a Civil Aircraft

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Abstract

To accelerate the design phases of the antiskid control system for a turboprop aircraft and to effectively ensure appropriate results, a brake-by-wire antiskid control system for a business aircraft is designed and investigated using a new virtual prototy** technology, which significantly reduces time, effort and cost. In contrast to traditional empirical formula methods, a multidisciplinary modeling co-simulation method has been proposed in this paper. The mathematical modeling process and antiskid control algorithm (Pressure Bias Modulation–Proportional–Integral Derivative) were analyzed and adopted. The co-simulation model was designed based on multi-body dynamic and multidisciplinary approach. The simulation results were compared with measured data sampled from an inertial platform test rig. The simulation results and physical experiment results proved the efficiency of the overall system.

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Data availability statement

The data that support the findings of this study are available on request from the corresponding author, upon reasonable request.

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Authors and Affiliations

  1. Key Laboratory of High-Efficiency and Clean Mechanical Manufacture of Ministry of Education, School of Mechanical Engineering, National Demonstration Center for Experimental Mechanical Engineering Education (Shandong University), Shandong University, **an, China

    Dawei Li & Mingxing Lin

  2. Aviation Industry Corporation of China, AVIC XI’AN Aircraft Industry (Group) Company LTD., **’an, China

    Dawei Li

  3. Aviation Industry Corporation of China, AVIC XAC Commercial Aircraft Co., LTD., **’an, China

    Tao Zhang

Authors
  1. Dawei Li
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  2. Mingxing Lin
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  3. Tao Zhang
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Correspondence to Mingxing Lin.

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Li, D., Lin, M. & Zhang, T. Design and Co-simulation of an Antiskid Brake System for a Civil Aircraft. Int. J. Aeronaut. Space Sci. 24, 845–852 (2023). https://doi.org/10.1007/s42405-022-00555-3

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  • DOI: https://doi.org/10.1007/s42405-022-00555-3

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