نمایش نتایج جستجو برای
نویسنده: امین آدینه اهری
موارد یافت شده: 4
1 - Design of Three-Dimensional Missile Guidance Law via Sliding Mode with Saturation Constraint (چکیده)2 - Dynamic Matrix Flight Control design for a nonlinear missile Autopilot (چکیده)
3 - Innovative Hybrid Backward Input Estimation and Data Fusion for High Maneuvering Target Tracking (چکیده)
4 - A New Missile Guidance Law Design based on Interception Point Strategy and Fuzzy Logic against High Maneuvering Targets (چکیده)
