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Optimal Maneuvers with Bounded Inputs

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

Abstract

Spacecraft engines can generate only limited thrust magnitudes. This implies that the acceleration inputs in space navigation must necessarily be bounded. The trajectory optimization must therefore be performed taking bounded inputs into account. As discussed in the earlier chapters, the nature of optimal trajectories with bounded acceleration inputs can be classified as either impulsive thrust or continuous thrust maneuvers.

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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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