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Aircraft anti-skid braking control based on pressure servo control using high-speed on/off valve

  • Beihang University
  • Beijing Institute of Precise Mechatronics and Controls

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In order to optimize one UAV current braking system, a new aircraft anti-skid braking system based on pressure servo control using high-speed on/off valves driven by PWM signals is proposed in this paper. The operation principle of PWM on/off valves is analyzed in details to prove the feasibility of pressure servo control. The brake controller contains pressure and slip ratio two closed loops to achieve accurate control and provide high stability. Experimental results show that the new system indeed improve the braking performance and efficiency.

Original languageEnglish
Title of host publicationCGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1369-1374
Number of pages6
ISBN (Electronic)9781467383189
DOIs
StatePublished - 20 Jan 2017
Event7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China
Duration: 12 Aug 2016 → 14 Aug 2016

Publication series

NameCGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/TerritoryChina
CityNanjing, Jiangsu
Period12/08/16 → 14/08/16

Keywords

  • Aircraft anti-skid braking
  • High-speed on/off valve
  • PWM
  • Pressure servo control

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