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针对国产某型号高速歼击机的数学模型及其数字式三轴电传操纵控制增稳系统，采用经典控制理论的方法，在数字式三轴电传操纵控制增稳系统的基础上，分析、设计了一种复杂的非线性控制系统──空－空机炮模态的综合火力／飞行控制系统．文中给出了该控制系统的构成，讨论了火力／飞行耦合器的结构．数学仿真表明，所设计的综合火力／飞行控制系统具有良好的性能，由于采用的飞机数学模型及其数字式三轴电传操纵控制增稳系统的真实性，使得所设计的综合火力／飞行控制系统具有较强的实际意义和工程使用价值．
According to the mathematical model of a domestic high-speed fighter and its digital three-axis transmission control augmentation system, based on the classical three-axis transmission control augmentation system based on classical control theory, this paper analyzes and designs A COMPETITIVE NONLINEAR CONTROL SYSTEM - INTEGRATED FIRE / FLIGHT CONTROL SYSTEM FOR AIR / CANON MODEL. The paper presents the structure of the control system and discusses the structure of the fire power / flight coupler. The mathematical simulation shows that the proposed integrated fire / flight control system has good performance. Due to the authenticity of the augmentation system controlled by the mathematical model of the aircraft and its digital triaxial telex, the integrated fire / flight control The system has strong practical significance and engineering value.