结合 发表于 2025-3-23 10:59:02

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Clinch 发表于 2025-3-23 15:38:04

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Confound 发表于 2025-3-23 18:17:19

Control Engineeringhttp://image.papertrans.cn/o/image/702923.jpg

Firefly 发表于 2025-3-24 01:24:20

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声明 发表于 2025-3-24 06:02:56

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maudtin 发表于 2025-3-24 10:00:20

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

有发明天才 发表于 2025-3-24 11:45:41

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

舰旗 发表于 2025-3-24 15:00:37

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宿醉 发表于 2025-3-24 19:00:57

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.

美丽的写 发表于 2025-3-25 03:15:25

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