نمایش نتایج جستجو برای
کلمات کلیدی: missile
موارد یافت شده: 5
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 - Design Controller H∞H2, LQG and predictive and for a jet transport aircraft (چکیده)
4 - Synthesis of robust PID controller for controlling a single input single output system using quantitative feedback theory technique (چکیده)
5 - Robust Controller Design for Missile Yaw Channel (چکیده)
