インフライトシミュレータMuPAL-αの横/方向運動モデルマッチング制御器の飛行実験(<小特集>運動と振動の制御の21世紀への新展開)

概要

論文の詳細を見る
In this paper, flight controller design for the lateral/direction motions of in-flight simulator MuPAL-α is discussed. For the simultaneous simulation of gust responses and pilot input responses of model aircraft, feedback and feed forward controllers are designed in two steps; feedback controllers for robust model-matching problem are first designed using scaled H_∞ control to simulate the gust responses of target aircraft, and then feed forward controllers for H_∞, model-matching are designed as right inverse systems to simulate the aircraft responses driven by pilot inputs. In the feedback controller design, we use airspeed in stead of inertial speed which was used in our previous report. After confirming that designed controllers have good model-matching performance with numerical simulations, we conducted hardware-in-the-loop simulations and flight tests. In the flight tests, we confirmed that controllers with air speed feedback have better model-matching performance than controllers with inertial speed feedback, i.e. we have improved the model-matching performance of in-flight simulator MuPAL-α for its lateral/directional motions.
社団法人日本機械学会の論文
2006-09-25