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Design of 3D Guidance Law for Tactical Missiles

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Proceedings of the International Conference on Modern Research in Aerospace Engineering

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

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Abstract

In this work, design of three-dimensional (3D) proportional navigation guidance law based on input-output linearization (IOL) for tactical missiles is proposed. For the three-dimensional nonlinear missile-target engagement dynamics, the line-of-sight (LOS) rates in pitch and yaw planes are taken as outputs and the IOL theory is used to derive the guidance laws without ignoring the cross-coupling terms. Simulations are carried out by considering maneuvering target, and the results are presented to showcase the efficacy of the proposed design. Further, comparison of the performance of the proposed guidance law with augmented proportional navigation guidance(APNG) laws is carried out and the related results are presented. Lastly, implementation issues of the proposed guidance law are discussed.

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Author information

Authors and Affiliations

  1. Department of Aerospace Engineering, Defence Institute of Advance Technology, Girinagar, 411025, Pune, India

    Sikander Kumar Pandit, Bhavnesh Panchal & S. E. Talole

Authors
  1. Sikander Kumar Pandit
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  2. Bhavnesh Panchal
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  3. S. E. Talole
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Corresponding author

Correspondence to Sikander Kumar Pandit .

Editor information

Editors and Affiliations

  1. Amity Institute of Aerospace Engineering, Amity University, Noida, Uttar Pradesh, India

    Sanjay Singh

  2. DTC Secretariat, Ghaziabad, Uttar Pradesh, India

    Pushkar Raj

  3. Department of Aerospace Engineering and Engineering Mechanics, College of Engineering and Applied Sciences, University of Cincinnati, Cincinnati, Ohio, USA

    Samir Tambe

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Pandit, S.K., Panchal, B., Talole, S.E. (2018). Design of 3D Guidance Law for Tactical Missiles. In: Singh, S., Raj, P., Tambe, S. (eds) Proceedings of the International Conference on Modern Research in Aerospace Engineering. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-10-5849-3_7

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  • DOI: https://doi.org/10.1007/978-981-10-5849-3_7

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-5848-6

  • Online ISBN: 978-981-10-5849-3

  • eBook Packages: EngineeringEngineering (R0)

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