OPEN DESIGN FOR HELICOPTER ACTIVE CONTROL SYSTEMS

著录项

• 来源
  《American Helicopter Society Flight controls and crew systems design technical specialists' meeting》|2002年|p.1-20|共20页
• 会议地点 Philadelphia PA(US)
• 作者

  Geoffrey J. Jeram;

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• 作者单位

  School of Aerospace Engineering Georgia Institute of Technology Atlanta, Georgia;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 V275.1;
• 关键词

  f, g, h: Vector functions; F: Vector of active control axes counter forces from the active inceptor to the pilot,F = F_(col) F_(long) F_(lat) F_(pedl) ~T; u: Control vector of k elements u = δ_1 δ_2 …δ_k ~T; x: Aircraft State Vector of n elements x = x_1 x_2 x_3 … x_n ~T; y: Aircraft Limit Vector of m elements y = y_1 y_2 y_3 …y_m ~T; et al;

  机译：f，g，h：矢量函数； F：活动控制轴的矢量抵抗从活动感受器到飞行员的力，F = [F_（col）F_（long）F_（lat）F_（pedl）]〜T； ; u：k个元素的控制向量u = [δ_1δ_2…δ_k]〜T ;; x：n个元素的飞机状态向量x = [x_1 x_2 x_3…x_n]〜T ;; y：m个元素y的飞机极限向量= [y_1 y_2 y_3…y_m]〜T ;;等;