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Titlebook: Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems; Runqi Chai,Al Savvaris,Senchun Chai Book 2020 S

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31#
發(fā)表于 2025-3-26 22:31:25 | 只看該作者
Multi-objective Trajectory Optimization Problem,ous-time optimal control model. Because of the discontinuity or nonlinearity in the vehicle dynamics and mission objectives, it is challenging to generate a compromised trajectory that can satisfy constraints and optimize objectives. To effectively analyze the relationships between objectives and ca
32#
發(fā)表于 2025-3-27 02:17:26 | 只看該作者
33#
發(fā)表于 2025-3-27 06:01:32 | 只看該作者
34#
發(fā)表于 2025-3-27 13:24:43 | 只看該作者
Book 2020cecraft trajectory optimization is one of the book’s major features, making it particularly suited for readers who are seeking practical solutions in spacecraft trajectory optimization. It offers a valuable asset for researchers, engineers, and graduate students in GNC systems, engineering optimizat
35#
發(fā)表于 2025-3-27 16:12:38 | 只看該作者
Multi-objective Trajectory Optimization Problem,more, in order to take into account the preference requirements, different transformation techniques are also proposed and the original problem is then transcribed to a single-objective formulation. These techniques are discussed in detail in the following sections. Numerical simulations were carrie
36#
發(fā)表于 2025-3-27 18:31:18 | 只看該作者
37#
發(fā)表于 2025-3-27 22:06:09 | 只看該作者
38#
發(fā)表于 2025-3-28 03:16:42 | 只看該作者
39#
發(fā)表于 2025-3-28 06:28:37 | 只看該作者
https://doi.org/10.1057/9780230295186more, in order to take into account the preference requirements, different transformation techniques are also proposed and the original problem is then transcribed to a single-objective formulation. These techniques are discussed in detail in the following sections. Numerical simulations were carrie
40#
發(fā)表于 2025-3-28 13:22:26 | 只看該作者
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