期刊:IEEE Transactions on Aerospace and Electronic Systems [Institute of Electrical and Electronics Engineers] 日期:2019-09-25卷期号:56 (3): 2122-2135被引量:17
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.