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