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邵晓巍
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[1]shaoxiaowei. Multi-spacecraft attitude cooperative control using model-based event-triggered methodology ADVANCES IN SPACE RESEARCH, 2018,
[2]shaoxiaowei. Kalman filtering through the feedback adaption of prior error covariance SIGNAL PROCESSING, 2018,
[3]shaoxiaowei. Stochastic Feedback Based Kalman Filter for Nonlinear Continuous-Discrete Systems IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2018,
[4]shaoxiaowei. Robust model predictive control for multi-step short range spacecraft rendezvous ADVANCES IN SPACE RESEARCH, 2018,
[5]shaoxiaowei. Learning observer based and event-triggered control to spacecraft against actuator faults AEROSPACE SCIENCE AND TECHNOLOGY, 2018,
[6]shaoxiaowei. Neural-Network-Based Sliding-Mode Adaptive Control for Spacecraft Formation Using Aerodynamic Forces JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS, 2018,
[7]shaoxiaowei. Neural network-based sliding mode control for atmospheric-actuated spacecraft formation using switching strategy ADVANCES IN SPACE RESEARCH, 2018,
[8]shaoxiaowei. Fault-tolerant adaptive finite-time attitude synchronization and tracking control for multi-spacecraft formation AEROSPACE SCIENCE AND TECHNOLOGY, 2018,
[9]shaoxiaowei. Multi-objective optimization method for repeat ground-track orbit design considering the orbit injection error JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT, 2018,
[10]shaoxiaowei. Optimal small satellite orbit design based on robust multi-objective optimization method AEROSPACE SCIENCE AND TECHNOLOGY, 2017,
[11] H∞ cross-coupled algorithm-based robust synchronous control in large dual-drive gantry stages International Journal of Automation & Control, 2017,
[12] Roto-translational spacecraft formation control using aerodynamic forces JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS, 2017,
[13] Modified fuel-balanced formation keeping strategy based on actively rotating satellites in formation AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017,
[14] A novel relative navigation method based on thrust on-line identification for tight formation keeping AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017,
[15] 基于H_∞-交叉耦合算法的双驱同步控制 浙江大学学报(工学版), 2017,
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