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Design of 3D Guidance Law for Tactical Missiles

  • Sikander Kumar Pandit
  • Bhavnesh Panchal
  • S. E. Talole
Conference paper
Part of the Lecture Notes in Mechanical Engineering book series (LNME)

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.

Keywords

3D guidance Input-output linearization Cross-coupling effects Missile guidance 

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Copyright information

© Springer Nature Singapore Pte Ltd. 2018

Authors and Affiliations

  • Sikander Kumar Pandit
    • 1
  • Bhavnesh Panchal
    • 1
  • S. E. Talole
    • 1
  1. 1.Department of Aerospace EngineeringDefence Institute of Advance TechnologyGirinagarIndia

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