论文信息 - Robust Flight Control System Design Using Discrete Time Utmost Compensator - 字舞流文

Robust Flight Control System Design Using Discrete Time Utmost Compensator

Morio Takahama | Takashi Kimura | Ryozaburo Tagawa | Ei Tokuda

[1] Ching-Fang Lin,et al. Robust missile autopilot design using a generalized singular optimalcontrol technique , 1985 .

[2] J. Ackermann. Robust Flight Control System Design , 1981 .