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Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2 H∞ Control

소개글 Author: Won Dae-Yeon, Tahk Min-Jea, Kim Yoon-Hwan Organization: Won Dae-Yeon; Tahk Min-Jea; Kim Yoon-Hwan Publish: International Journal Aeronautical and Space Sciences Volume 11, Issue2, p131~135, 15 June 2010
태그
  • Mixed H2/H∞ control
  • Three-axis autopilot
  • Linear matrix inequality technique