大连理工大学主页平台管理系统彭海军--中文主页-- Surrogate-based Parameter Optimization and Optimal Control for Optimal Trajectory of Halo Orbit Rendezvous

论文成果

Surrogate-based Parameter Optimization and Optimal Control for Optimal Trajectory of Halo Orbit Rendezvous

上一条：基于SiPESC平台的卫星编队飞行视景仿真系统设计和实现

下一条： Precise Integration Method for Solving Noncooperative LQ Differential Game

彭海军 var u_u6_pic = new ImageScale("u_u6_",140,140,true,true);u_u6_pic.addimg("/_resources/group1/M00/00/1B/ynZMg18RfaOAXiHBAADw4hRY7Ag129.JPG","","彭海军","7356");