Titlebook: Space Engineering; Modeling and Optimiz Giorgio Fasano,János D. Pintér Book 2016 Springer International Publishing Switzerland 2016 Balanci

拖累

书目名称Space Engineering影响因子(影响力)




书目名称Space Engineering影响因子(影响力)学科排名




书目名称Space Engineering网络公开度




书目名称Space Engineering网络公开度学科排名




书目名称Space Engineering被引频次




书目名称Space Engineering被引频次学科排名




书目名称Space Engineering年度引用




书目名称Space Engineering年度引用学科排名




书目名称Space Engineering读者反馈




书目名称Space Engineering读者反馈学科排名

Metamorphosis

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

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

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

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

Hemiplegia

Magnificent

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

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