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  1. No Access

    Chapter and Conference Paper

    Design and Analysis of Missile Two-Loop Autopilot with Angle of Attack Feedback

    In order to eliminate the static error of the classic two loop autopilot, the PI compensator is introduced into the control system. To enhance the robustness of two loop autopilot with PI compensator, an angle...

    Jiang Wang, Zhe Yang, De-fu Lin in System Simulation and Scientific Computing (2012)

  2. No Access

    Chapter and Conference Paper

    Computing Stability for Autopilots Based on Vector Margin

    A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All ava...

    Jiang Wang, De-fu Lin, Jun-fang Fan in Future Control and Automation (2012)