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Two-Body Maneuvers with Unbounded Continuous Inputs

  • Ashish Tewari
Chapter
Part of the Control Engineering book series (CONTRENGIN)

Abstract

A majority of spacecraft navigation problems involve transfers between two given positions and velocities. When continuous inputs are applied for the orbital transfer of a spacecraft around a central body, the perturbed two-body model can be used as a plant to derive the optimal trajectory and control history.

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Copyright information

© Springer Nature Switzerland AG 2019

Authors and Affiliations

  • Ashish Tewari
    • 1
  1. 1.Department of Aerospace EngineeringIndian Institute of Technology, KanpurIIT-KanpurIndia

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