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Model Predictive Control for A Missile with Blended Lateral Jets and Aerodynamic Fins
  • 所属机构名称：哈尔滨工业大学
  • 会议名称：27th Chinese Control Conference
  • 成果类型：会议
  • 会场：Kunming, PEOPLES R CHINA
  • 相关项目：基于混杂系统理论的蜂群式协同拦截策略研究
作者： Yang Baoqing|He Fenghua|Yao Yu|Ma Kemao|
同会议论文项目
基于混杂系统理论的蜂群式协同拦截策略研究
期刊论文 23 会议论文 11
同项目会议论文
Simultaneous Attitude Stabilization and Power Tracking for a Spacecraft with Two VSCMGs
Firing Logic Optimization Design of Lateral Jets in Missile Attitude Control Systems
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Blended Control System Design for Agile Missile with Lateral Jets and Aerodynamic Surfaces
Attitude Stabilization of Spacecraft with Two Moving-Mass Via Interconnection and Damping Assignment
Switching Logic Design Based on Finite-Time Gain Measure for A Flight Vehicle with Multiple Actuator
大气层内直接侧向力控制拦截导弹末段修正能力分析
Logic-based Switching Control Strategy Design of a Spinning Missile with Blended Lateral Jets and Ae
Attitude stabilization of an under-actuated rigid spacecraft via logic-based switching control
Finite-time H-2 Performance Analysis Considering Target Maneuvers and Guidance Loop Dynamics