飞机
控制理论(社会学)
飞行模拟器
控制器(灌溉)
航程(航空)
工程类
空气动力学
飞行动力学
飞行试验
计算机科学
模拟
控制工程
航空航天工程
控制(管理)
农学
人工智能
生物
标识
DOI:10.1109/taes.2019.2943770
摘要
In-Flight Simulators (IFSs) require flight controllers, which mimic other aircraft's dynamics in a certain operation range, which is the problem addressed in this paper. The design problem of a linear parameter-varying type gain-scheduled flight controller, which simultaneously suppresses gust effect and reproduces low-and-middle frequency commands as IFS's motions in a certain speed range, for the lateral-directional motions of an airplane is addressed via linear matrix inequality formulation. Our controller performance is examined by flight tests.
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