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Modern Astrodynamics by Pini Gurfil

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6

Space Trajectory Optimization and L1-Optimal Control Problems

I. Michael Ross     Department of Mechanical and Astronautical Engineering, Naval Postgraduate School, Monterey, CA 93943.

6.1 Introduction

The engineering feasibility of a space mission is overwhelmingly dictated by the amount of propellant required to accomplish it. This requirement ...

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