Titlebook: Modelling and Simulation for Autonomous Systems; 6th International Co Jan Mazal,Adriano Fagiolini,Petr Vasik Conference proceedings 2020 Sp

浮標(biāo)

書目名稱Modelling and Simulation for Autonomous Systems影響因子(影響力)




書目名稱Modelling and Simulation for Autonomous Systems影響因子(影響力)學(xué)科排名




書目名稱Modelling and Simulation for Autonomous Systems網(wǎng)絡(luò)公開度




書目名稱Modelling and Simulation for Autonomous Systems網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Modelling and Simulation for Autonomous Systems被引頻次




書目名稱Modelling and Simulation for Autonomous Systems被引頻次學(xué)科排名




書目名稱Modelling and Simulation for Autonomous Systems年度引用




書目名稱Modelling and Simulation for Autonomous Systems年度引用學(xué)科排名




書目名稱Modelling and Simulation for Autonomous Systems讀者反饋




書目名稱Modelling and Simulation for Autonomous Systems讀者反饋學(xué)科排名

猛然一拉

0302-9743 utonomous Systems, MESAS 2019, held in Palermo, Italy, in October 2019...The 22 full papers and 13 short papers included in the volume were carefully reviewed and selected from 53 submissions. They are organized in the following topical sections: M&S of intelligent systems - AI, R&D and application;

厭煩

0302-9743 future challenges of advanced M&S technology; AxS in context of future warfare and security environment (concepts, applications, training, interoperability, etc.)..978-3-030-43889-0978-3-030-43890-6Series ISSN 0302-9743 Series E-ISSN 1611-3349

諷刺滑稽戲劇

性學(xué)院

Lecture Notes in Computer Sciencehttp://image.papertrans.cn/m/image/636618.jpg

dyspareunia

HALL

978-3-030-43889-0Springer Nature Switzerland AG 2020

integrated

Mast-Cell

Study on GEO Metaheuristic for Solving Multiprocessor Scheduling Problemown Simulated Annealing (SA) algorithm. Both algorithms have some similarities which are considered in this paper. Experimental results show that GEO despite of its simplicity outperforms SA algorithm in all range of the scheduling instances.

不整齊

Das Münzenproblem von Frobeniusa safety margin is not violated. The solution is a safe continuous trajectory that minimizes the distance covered. We present preliminary results assuming weather to be the only source of uncertainty. We consider an aircraft point-mass model at constant altitude and airspeed with manoeuvres being limited by a minimum turning radius.