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Design and Flight Testing of a Gain-Scheduled Autopilot Based on Reduced Model Constraints

机译:基于减少的模型约束的增益调度自动驾驶仪的设计与飞行测试

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The purpose of this paper focuses on the design, evaluation and flight testing of a gain-scheduled autopilot for a missile system based on reduced modelling constraints. The controller synthesis based on frequency response analysis theory formed the basis for the implementation of gain-scheduled controllers. During the controller synthesis process, the design constraints were based on a reduced missile model and analytically computed controller initial gains which improved the controller optimization phase while satisfying the robustness and performance requirements across the envisioned flight envelope. This process was shown to produce successful results in both a nonlinear desktop simulation and a flight testing campaign.
机译:本文的目的集中在基于减少的建模约束的导弹系统增益预定自动驾驶仪的设计,评估和飞行测试上。基于频率响应分析理论的控制器综合为实现增益调度控制器奠定了基础。在控制器综合过程中,设计约束基于简化的导弹模型和经过分析计算的控制器初始增益,从而改善了控制器优化阶段,同时满足了所设想的飞行范围内的鲁棒性和性能要求。该过程在非线性桌面仿真和飞行测试中均显示出成功的结果。

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