控制配置(Control Allocation)是多控制面戰鬥機中不可或缺的設計方法，隨著現代戰機對於作戰性能(如：高機動性、敏捷性、匿蹤能力)的要求提高，傳統布局的第四代戰機已無法滿足要求。第五代戰機多採用多控制面布局，除了氣動力控制面的數量增加外，推進系統的向量噴嘴也可當成控制面使用，大幅增加了控制面的數量，但也超出了飛行員的操縱能力。本論文提出控制配置的觀念，將控制系統拆分成控制律與分配律。控制系統中的控制律選用非線性動態反算，並獨立設計分配律。不同於傳統戰鬥機直接透過控制律產生控制面的偏轉指令，多控制面戰鬥機引入了分配律後，有效的避免控制面提早達到飽和，同時根據不同控制面偏轉造成的氣動力特性，有效的分配控制面偏轉。本論文引入系統力矩可達集(AMS)凸多面體的概念，探討廣義逆類配置法和幾何類配置法的配置效率，並透過六自由度模擬驗證不同配置法的優缺點。

Control Allocation is an indispensable design method in aircraft with multiple control surfaces. With the increasing requirements of modern fighters for combat performance (such as high mobility, agility, and stealth ability), the fourth-generation fighters with traditional layouts have been unable to meet the requirements. Fifth-generation fighters mostly use a multiple control surfaces layout. In addition to the increase in the number of aerodynamic control surfaces, the vectoring nozzles can also be used as control surfaces, which greatly increases the number of control surfaces and exceeds the pilot's control capabilities. This thesis proposes the concept of Control Allocation, splits the control system into control law and allocation law. The control law in the control system uses Nonlinear Dynamic Inverse and the allocation law is designed independently. Traditional aircraft directly generates control surface deflection commands through the control law. The aircraft with multiple control surfaces introduces allocation law, which effectively allocates the control surface deflection according to the aerodynamic characteristics of different control surfaces. Therefore, premature saturation of control surfaces can be avoided in the allocation law. This thesis introduces the concept of Attainable Moment Subset(AMS), discusses the allocation effectiveness of Generalized Inverse Allocation Methods and Geometric Allocation Methods. Finally, the advantages and disadvantages of allocation methods are verified through six-degree-of-freedom simulation.

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