拖累
发表于 2025-3-21 16:40:12
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Metamorphosis
发表于 2025-3-22 00:08:53
Using Direct Transcription to Compute Optimal Low Thrust Transfers Between Libration Point Orbits,hrust orbit transfer between libration point orbits. The recent implementation of high order discretization techniques is first described and then illustrated by computing optimal low thrust trajectories between orbits about the .. and .. Earth-Moon libration points.
磨坊
发表于 2025-3-22 00:27:11
Tentative Solutions for Indirect Optimization of Spacecraft Trajectories,s is discussed. The application of theory of optimal control to spacecraft trajectories transforms the optimal control problem into a multi-point boundary value problem, which is usually solved by means of an iterative procedure. The convergence radius of the problem may be small and convergence to
Limerick
发表于 2025-3-22 05:22:03
Resource-Constrained Scheduling with Non-constant Capacity and Non-regular Activities, optimizing the resource exploitation is discussed. The available resources are not constant, as well as the request, relative to each job. The mathematical aspects are illustrated, providing a time-indexed MILP model. The case of a single resource is analysed first. Extensions, including the multi-
短程旅游
发表于 2025-3-22 10:17:39
Packing Problems in Space Solved by CPLEX: An Experimental Analysis,eemed to become, day after day, ever more demanding in the perspective of the upcoming exploration adventures. Extremely thought provoking packing optimization problems have to be coped with, in the presence of intricate geometries, operational conditions and, usually, very tight balancing requireme
坚毅
发表于 2025-3-22 12:53:40
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Hemiplegia
发表于 2025-3-22 17:53:20
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Magnificent
发表于 2025-3-22 23:13:33
Re-entry Test Vehicle Configuration Selection and Analysis,veloped subsystems in a realistic environment. To establish the optimal vehicle shape a response-surface methodology using design-of-experiments techniques is proposed. With these techniques the effects of changing several geometric design parameters in an ‘all-at-the-same-time’ approach can be stud
指派
发表于 2025-3-23 01:25:02
Rigorous Global Optimization for Collision Risk Assessment on Perturbed Orbits,ed. The method is based on the computation of the minimum distance between two evolving orbits by means of a rigorous global optimizer. Analytical solutions of artificial satellite motion are utilized to account for perturbative effects of Earth’s zonal harmonics, atmospheric drag, and third body. I
Venules
发表于 2025-3-23 08:55:01
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