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Elsevier电子期刊(593)

在“Elsevier电子期刊”中，命中：593条，耗时：小于0.01 秒

在所有数据库中总计命中：593条

1.LEO cooperative multi-spacecraft refueling mission optimization considering J₂ perturbation and target’s surplus propellant constraint

作者：Zhao Zhao^a ; Jin Zhang^a ; ^{zhangjin@nudt.edu.cn} ; ^{zhangjinxy1983@gmail.com} ; Hai-yang Li^a ; Jian-yong Zhou^b

关键词：Cooperative refueling ; Rendezvous ; J2 perturbation ; Hybrid optimization ; Hybrid-encoding genetic algorithm ; MINLP

刊名：Advances in Space Research

出版年：2017

2.Shape-based analytic safe trajectory design for spacecraft equipped with low-thrust engines

作者：Kui Zeng ; Yunhai Geng ; Baolin Wu ; ^{wubaolin@hit.edu.cn}

关键词：Rapid trajectory design ; Shape-based approach ; Low-thrust trajectory ; Transfer and rendezvous problems

刊名：Aerospace Science and Technology

出版年：2017

3.Scalable multicasting with multiple shared trees in software defined networking

作者：Ying-Dar Lin^a ; Yuan-Cheng Lai^b ; Hung-Yi Teng^a ; ^{marstwng@gmail.com} ; Chun-Chieh Liao^a ; Yi-Chih Kao^c

关键词：Software defined networking ; Multiple shared trees ; Locality-aware ; Multicast clustering ; Rendezvous point

刊名：Journal of Network and Computer Applications

出版年：2017

4.Clinical Outcomes of Pedal Artery Angioplasty for Patients With Ischemic Wounds: Results From the Multicenter RENDEZVOUS Registry

作者：Tatsuya Nakama ; MD^a ; ^{tatsuya_nakama@med.miyazaki-u.ac.jp} ; Nozomi Watanabe ; MD^a ; Takuya Haraguchi ; MD^b ; Hiroshi Sakamoto ; MD^c ; Daisuke Kamoi ; MD^d ; Yoshinori Tsubakimoto ; MD^e ; Kenji Ogata ; MD^a ; Katsuhiko Satoh ; MD^b ; Kazushi Urasawa ; MD^b ; Hiroshi Andoh ; MD^c ; Hiroshi Fujita ; MD^e ; Yoshisato Shibata ; MD^a

关键词：below-the-ankle intervention ; critical limb ischemia ; endovascular therapy ; pedal artery diseases ; peripheral arterial diseases ; wound healing

刊名：JACC: Cardiovascular Interventions

出版年：2017

5.Automatic trajectory planning for low-thrust active removal mission in low-earth orbit

作者：Marilena Di Carlo ^{marilena.di-carlo@strath.ac.uk} ; Juan Manuel Romero Martin ^{juan.romero-martin@strath.ac.uk} ; Massimiliano Vasile ; ^{massimiliano.vasile@strath.ac.uk}

关键词：Active debris removal ; Orbital debris ; Debris mitigation ; Automated trajectory design ; Automatic planning and scheduling ; Low-thrust transfers

刊名：Advances in Space Research

出版年：2017

6.Rendezvous with constant memory

作者：P. Flocchini^a ; ^{pflocchi@uottawa.ca" class="auth_mail" title="E-mail the corresponding author} ; N. Santoro^b ; G. Viglietta^b ; M. Yamashita^c

关键词：Autonomous mobile robots ; Finite states robots ; Robots with lights ; Rendezvous ; Gathering ; Obliviousness and memory ; Synchrony vs. asynchrony

刊名：Theoretical Computer Science

出版年：2016

7.A periodic jump-based rendezvous algorithm in cognitive radio networks

作者：Saber Salehkaleybar ; ^{saber.salehk@gmail.com" class="auth_mail" title="E-mail the corresponding author} ; ^{saber_saleh@ee.sharif.edu" class="auth_mail" title="E-mail the corresponding author} ; Mohammad Reza Pakravan ^{pakravan@sharif.edu" class="auth_mail" title="E-mail the corresponding author}

关键词：Opportunistic Spectrum Access (OSA) ; Blind rendezvous ; Multichannel Medium Access Control (MAC) protocols

刊名：Computer Communications

出版年：2016

8.Optimization of an orbital long-duration rendezvous mission

作者：Jin Zhang ; ^{zhangjin@nudt.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; ^{zhangjinxy1983@gmail.com" class="auth_mail" title="E-mail the corresponding author} ; Guo-jin Tang ; Ya-zhong Luo

关键词：Orbital rendezvous ; Long-duration maneuvers ; Mixed integer nonlinear programming ; Engineering optimization

刊名：Aerospace Science and Technology

出版年：2016

9.Symplectic method based on generating function for receding horizon control of linear time-varying systems

作者：Haijun Peng^a ; ^{hjpeng@dlut.edu.cn} ; Shujun Tan^b ; Qiang Gao^a ; Zhigang Wu^b

关键词：Receding horizon control ; Generating functions ; Linear time-varying systems ; Hamiltonian systems ; Symplectic method

刊名：European Journal of Control

出版年：2017

10.Global fuel consumption optimization of an open-time terminal rendezvous and docking with large-eccentricity elliptic-orbit by the method of interval analysis

作者：Hongliang Ma^a ; ^{mahongliang317@sina.com" class="auth_mail" title="E-mail the corresponding author} ; Shijie Xu^b ; ^{starsjxu@163.com" class="auth_mail" title="E-mail the corresponding author}

关键词：Open-time ; Two-impulse ; Elliptical rendezvous docking ; Global optimization ; Interval analysis

刊名：Acta Astronautica

出版年：2016

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