Titlebook: Optimal Space Flight Navigation; An Analytical Approa Ashish Tewari Book 2019 Springer Nature Switzerland AG 2019 Orbital Space Mechanics.S

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Optimal Space Flight Navigation978-3-030-03789-5Series ISSN 2373-7719 Series E-ISSN 2373-7727

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Introduction,Navigating a space vehicle consists of first determining and then steering a desired path under the gravitational influence of several large bodies.

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Two-Body Maneuvers with Unbounded Continuous Inputs,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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