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Intelligent Communication, Control and Devices pp 393–400Cite as

Linear Flight Control of Unmanned Aerial Vehicle

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Part of the book series: Advances in Intelligent Systems and Computing ((AISC,volume 624))

Abstract

In this chapter, state feedback controller with the help of full state feedback method or pole placement technique is designed to stabilize the lateral dynamics of unmanned aerial vehicle (UAV). Poles of the system are chosen such that system’s performance meets the design specifications with the help of MATLAB. This chapter also analyzes the transient specifications.

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References

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Author information

Authors and Affiliations

  1. Electrical and Electronics Department, KIET, Ghaziabad, India

    Alok Kumar Pandey, Anshuman Shukla, Ashutosh Gupta & Manjeet Singh Gangwar

Authors
  1. Alok Kumar Pandey
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  2. Anshuman Shukla
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  3. Ashutosh Gupta
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  4. Manjeet Singh Gangwar
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Corresponding author

Correspondence to Alok Kumar Pandey .

Editor information

Editors and Affiliations

  1. Institute of Robotics Technology (R&D), University of Petroleum and Energy Studies, Dehradun, Uttarakhand, India

    Rajesh Singh

  2. Department of Electronics & Instrumentation Engineering, University of Petroleum and Energy Studies, Dehradun, Uttarakhand, India

    Sushabhan Choudhury

  3. Department of Electronics & Instrumentation Engineering, University of Petroleum and Energy Studies, Dehradun, Uttarakhand, India

    Anita Gehlot

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Cite this paper

Pandey, A.K., Shukla, A., Gupta, A., Gangwar, M.S. (2018). Linear Flight Control of Unmanned Aerial Vehicle. In: Singh, R., Choudhury, S., Gehlot, A. (eds) Intelligent Communication, Control and Devices. Advances in Intelligent Systems and Computing, vol 624. Springer, Singapore. https://doi.org/10.1007/978-981-10-5903-2_40

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  • DOI: https://doi.org/10.1007/978-981-10-5903-2_40

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-5902-5

  • Online ISBN: 978-981-10-5903-2

  • eBook Packages: EngineeringEngineering (R0)

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