Skip to main content

Concept of Automatic Landing Gear System with Altitude and Distance as Parameters

  • Conference paper
  • First Online:
Proceedings of International Conference on Cognition and Recognition

Part of the book series: Lecture Notes in Networks and Systems ((LNNS,volume 14))

  • 745 Accesses

Abstract

Aircraft’s landing gear, controlled by the pilots, helps the aircraft both at take-off and landing. In this paper the concept of automatic landing gear is been presented by taking the input data from the altimeter and Distance measuring equipment. This concept eases pilot control and reduces human error. The modeling of the system with replication of extraction and retraction of landing gear for three special cases is been done using servos with the help of PSoC micro-controller and the flowchart describes the logic of the program.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 169.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Hawkins M, Jr Willis (1954) Aircraft landing gear mechanism. US patent 269088

    Google Scholar 

  2. Che J, Chen D (2001) Automatic landing control using H∞ control and stable inversion. In: Proceedings of 40th IEEE conference on decision and control, Orlando, Florida, USA

    Google Scholar 

  3. Kaneshige J, Gundy Burlet K (2001) Integrated neural flight and propulsion control system. In: AIAA guidance, navigation and control conference

    Google Scholar 

  4. Oishi M, Mitchell I, Bayen A, Tomlin C (2002) Hybrid verification of an interface for an automatic landing. In: Proceedings of 41st IEEE conference on decision and control, Las Vegas, CA

    Google Scholar 

  5. Miller JH, Norfolk (1951) Automatic control system for aircraft retractable landing gear. US patent 2580452

    Google Scholar 

  6. Nebylov A, Sharan S (2007) Comparative analysis of design variants for low altitude flight parameters measuring system. In: 17th IFAC symposium for automatic control

    Google Scholar 

  7. Dimitri L (1975) Distance measuring equipment for aircraft employing precision distance measuring means. US patent 3870993

    Google Scholar 

  8. Bollard RJ, Feintuch M, Johnston RJ (1989) Integrated avionics control and display arrangement. US patent 4845495

    Google Scholar 

  9. PSoC http://www.cypress.com/?rID=72824

  10. Miniprog 3 http://www.cypress.com/?docID=44358

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Eshaan M. Khanapuri .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2018 Springer Nature Singapore Pte Ltd.

About this paper

Cite this paper

Khanapuri, E.M., Rao, M. (2018). Concept of Automatic Landing Gear System with Altitude and Distance as Parameters. In: Guru, D., Vasudev, T., Chethan, H., Kumar, Y. (eds) Proceedings of International Conference on Cognition and Recognition . Lecture Notes in Networks and Systems, vol 14. Springer, Singapore. https://doi.org/10.1007/978-981-10-5146-3_7

Download citation

  • DOI: https://doi.org/10.1007/978-981-10-5146-3_7

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-5145-6

  • Online ISBN: 978-981-10-5146-3

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics