標(biāo)題: Titlebook: Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems; Runqi Chai,Al Savvaris,Senchun Chai Book 2020 S [打印本頁] 作者: Espionage 時間: 2025-3-21 19:54
書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems影響因子(影響力)
書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems影響因子(影響力)學(xué)科排名
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書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems被引頻次
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書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems讀者反饋
書目名稱Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems讀者反饋學(xué)科排名
作者: prediabetes 時間: 2025-3-21 23:36 作者: Coronation 時間: 2025-3-22 01:42
https://doi.org/10.1057/9781137522023near constrained optimal control model is established. The constructed formulation contains multiple exo-atmospheric and atmospheric flight phases and correspondingly, two sets of flight dynamics. In addition, in order to guide the SMV overflying different target altitude points, a series of event s作者: 勛章 時間: 2025-3-22 07:16
Sarajevo: Sunday, June 28, 1914on the performance analysis, one may be able to improve one of these techniques in order to circumvent the limitations brought by the classic methods. In the analysis, two types of optimization strategies are applied to solve the SMV trajectory optimization problem. Specifically, gradient-based and 作者: GUISE 時間: 2025-3-22 12:16
Labour Market Policies in Times of Crisisof the initial guess and enhance the stability of the algorithm, an initial guess generator based on a specific stochastic algorithm is applied. In addition, an improved gradient-based algorithm is used as the inner solver, which can offer the user more flexibility to control the optimization proces作者: misshapen 時間: 2025-3-22 15:03 作者: misshapen 時間: 2025-3-22 18:07 作者: EWE 時間: 2025-3-22 21:41 作者: 工作 時間: 2025-3-23 01:55
https://doi.org/10.1007/978-981-13-9845-2Spacecraft; Trajectory optimization; Optimal control; Gradient-based approach; Heuristic method; Optimal 作者: 聰明 時間: 2025-3-23 07:26 作者: 痛打 時間: 2025-3-23 11:46 作者: surmount 時間: 2025-3-23 15:39 作者: 圖表證明 時間: 2025-3-23 21:54
Springer Aerospace Technologyhttp://image.papertrans.cn/d/image/268778.jpg作者: vector 時間: 2025-3-24 01:38
1869-1730 ation strategy.Presents new multi-objective approaches to fiThis book explores the design of optimal trajectories for space maneuver vehicles (SMVs) using optimal control-based techniques. It begins with a comprehensive introduction to and overview of three main approaches to trajectory optimization作者: forbid 時間: 2025-3-24 02:54
Book 2020rehensive introduction to and overview of three main approaches to trajectory optimization, and subsequently focuses on the design of a novel hybrid optimization strategy that combines an initial guess generator with an improved gradient-based inner optimizer. Further, it highlights the development 作者: 寬容 時間: 2025-3-24 07:04 作者: intercede 時間: 2025-3-24 13:49
https://doi.org/10.1057/9781137522023chnique is applied to discretize the continuous-time system. Initial simulations and different case studies are carried out. The obtained results reveal that it is feasible to use the proposed multi-phase optimal control formulation for fulfilling the multi-phase SMV skip entry mission.作者: Yourself 時間: 2025-3-24 16:04 作者: 上釉彩 時間: 2025-3-24 22:39
Labour Market Policies in Times of Crisisf convergence speed and convergence ability, when compared with other typical optimal control solvers. A Monte Carlo simulation was performed and the results show a robust performance of the proposed algorithm in dispersed conditions.作者: exceed 時間: 2025-3-25 01:28 作者: obsession 時間: 2025-3-25 04:06 作者: reflection 時間: 2025-3-25 11:12 作者: shrill 時間: 2025-3-25 15:10
Hybrid Optimization Methods with Enhanced Convergence Ability,f convergence speed and convergence ability, when compared with other typical optimal control solvers. A Monte Carlo simulation was performed and the results show a robust performance of the proposed algorithm in dispersed conditions.作者: 懶洋洋 時間: 2025-3-25 16:43
From the First World War to the Arab Springcecraft skip entry mission scenarios are also introduced. Following that, the overall aims and objectives of the book will be summarized. Finally, the structure of the entire book, together with some highlights of each chapter, will be given.作者: GIDDY 時間: 2025-3-25 23:23
Introduction,cecraft skip entry mission scenarios are also introduced. Following that, the overall aims and objectives of the book will be summarized. Finally, the structure of the entire book, together with some highlights of each chapter, will be given.作者: HALO 時間: 2025-3-26 02:33
Introduction,idance and control of the space vehicle. Among these flight missions, trajectory optimization for reentry vehicles is usually recognized as a challenging problem and it has been widely researched for a couple of decades. One of the current objectives is the development of space maneuver vehicles for作者: FOR 時間: 2025-3-26 08:00
Overview of Trajectory Optimization Techniques,fically, the main focus will be on the recently proposed optimization methods that have been utilized in constrained trajectory optimization problems and multi-objective trajectory optimization problems. An overview regarding the development of optimal control methods is first introduced. Following 作者: constellation 時間: 2025-3-26 08:41
Modeling of the Trajectory Optimization Problems,near constrained optimal control model is established. The constructed formulation contains multiple exo-atmospheric and atmospheric flight phases and correspondingly, two sets of flight dynamics. In addition, in order to guide the SMV overflying different target altitude points, a series of event s作者: 鞠躬 時間: 2025-3-26 13:41
Performance Analysis of Different Optimization Strategies,on the performance analysis, one may be able to improve one of these techniques in order to circumvent the limitations brought by the classic methods. In the analysis, two types of optimization strategies are applied to solve the SMV trajectory optimization problem. Specifically, gradient-based and 作者: Resign 時間: 2025-3-26 18:02
Hybrid Optimization Methods with Enhanced Convergence Ability,of the initial guess and enhance the stability of the algorithm, an initial guess generator based on a specific stochastic algorithm is applied. In addition, an improved gradient-based algorithm is used as the inner solver, which can offer the user more flexibility to control the optimization proces作者: attenuate 時間: 2025-3-26 22:31
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作者: infarct 時間: 2025-3-27 02:17 作者: 灌輸 時間: 2025-3-27 06:01 作者: 樂章 時間: 2025-3-27 13:24
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作者: 膝蓋 時間: 2025-3-27 16:12
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作者: 爆炸 時間: 2025-3-27 18:31 作者: Concrete 時間: 2025-3-27 22:06 作者: insecticide 時間: 2025-3-28 03:16 作者: 培養(yǎng) 時間: 2025-3-28 06:28
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作者: Manifest 時間: 2025-3-28 13:22 作者: Bereavement 時間: 2025-3-28 15:56
Techniques of Learning Temperature Change-constraint-handling strategy can outperform other existing approaches analyzed in this study, and the developed computational framework can produce reliable and less conservative solutions for the chance-constrained stochastic spacecraft trajectory planning problem. We hope that by reading this sec作者: Malfunction 時間: 2025-3-28 19:24
