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分析了反馈线性化飞行控制的奇异摄动降阶条件，讨论了外环解耦矩阵的奇异域和跟踪误差，建立了操纵面冗余时分配偏转指令的原则。用过失速转弯等机动进行了数值仿真验证。
The singular perturbation reduction conditions of feedback linearized flight control are analyzed. The singularity and tracking error of the outer loop decoupling matrix are discussed. The principle of assigning deflection commands when the control plane is redundant is established. The results of numerical simulations using maneuvers such as stalling and cornering.