The paper designed aerodynamic control system of pith and yaw channels and roll angle stabilization system, by using unsteady-state error follow-up control theory and state observation station theory in modern control theory.
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- 本文使用現代控制理論中的無(wú)靜差跟蹤控制系統理論與狀態(tài)觀(guān)測器理論，設計了俯仰、偏航兩個(gè)通道的氣動(dòng)力控制系統和滾轉角穩定系統。
